Development of lumped-parameter mathematical models for a vehicle localized impact

Size: px
Start display at page:

Download "Development of lumped-parameter mathematical models for a vehicle localized impact"

Transcription

1 Journal of Mechanical Science and Technology 5 (7) () 737~747 DOI.7/s6--55-x Developent of luped-paraeter atheatical odels for a vehicle localized ipact Witold Pawlus, Haid Reza Karii * and Kjell Gunnar Robbersyr Departent of Engineering, Faculty of Engineering and Science, University of Agder, N-4898 Gristad, Norway (Manuscript Received October 5, ; Revised March 5, ; Accepted March 5, ) Abstract In this paper, we propose a ethod of odeling for vehicle crash systes based on viscous and elastic properties of the aterials. This paper covers an influence of different arrangeent of spring and daper on the odels response. Differences in siulating vehicle-torigid barrier collision and vehicle-to-pole collision are explained. Coparison of the odels obtained fro wideband (unfiltered) acceleration and filtered acceleration is done. At the end we propose a odel which is suitable for localized collisions siulation. Keywords: Data analysis; Filtering; Modeling; Vehicle crash Introduction This paper deals with establishing an appropriate atheatical odel representing vehicle soft ipacts such as localized pole collisions. In siulation of the vehicle collision, eleents which exhibit viscous and elastic properties are used. Models utilized by us consist of energy absorbing eleents (EA) and asses connected to their both ends. We focus on finding a odel with such an arrangeent of springs, dapers and asses, which siulated, will give a response siilar to the car's behavior during the real crash. Due to the fact that real crash tests are coplex and coplicated events, their odeling is justified and advisable. Every car which is going to appear on the roads has to confor to the worldwide safety standards. However, crash tests consue a lot of effort, tie and oney. The appropriate equipent and qualified staff is needed as well. Therefore our goal is to ae possible siulation of a vehicle crash on a personal coputer. When it coes to odeling the vehicle crash we can distinguish two ain approaches. The first one utilizes CAE (Coputer Aided Engineering) software including FEA (Finite Eleent Analysis) while the second one bases on the analytical ethod presented in this paper. Much research has been done so far in both of those areas. Refs. [-3] provide a brief overview of different types of vehicle collisions. This paper was recoended for publication in revised for by Associate Editor Mohaad Abdul Aziz Irfan * Corresponding author. Tel.: , Fax.: E-ail address: haid.r.arii@uia.no KSME & Springer Approach presented here - atheatical odeling of a crash event with the equations of otion which can be solved explicitly with closed for solutions - is different that the ethods which have been shown in Refs. [4-7]. In order to siulate the collision of a car the software based on FEM (Finite Eleent Method) was utilized. After the creation of 3D CAD and FE odels, the crash siulations were perfored. Results obtained showed good correlation between the test and odel responses. When it coes to deterining crush stiffness coefficients, in Ref. [8] it is presented a ethod which eploys CRASH3 coputer progra. Vehicle structure was odeled as a hoogenous body and then the coparative analysis of the crash response of vehicles tested in both: full-overlap and partial-overlap collisions, was done. A luped paraeter odeling (LPM) is another way of approxiation of the vehicle crash. It is an analytical ethod of forulating a odel which can be further used for siulation of a real event. It allows us to establish dynaic equations of the syste - differential equations - which give the coplete description of the odel's behavior, see Refs. [9] and []. To be able to create a atheatical odel of a vehicle collision, it is often enough (and ore efficient) not to analyze the coplicated crash pulse recorded during the full-scale experient but just to study an approxiation of the easured acceleration signal. Those approxiated functions were copared to experiental pulses in Ref. []. Subsequently they were tested to obtain different odels' responses which were copared to the original pulse. Results confired that the crash pulse approxiation is a reasonable ethod to siplify the collision analysis. Recently, the Haar wavelet-based perforance analysis of the safety barrier for use in a full-scale

2 738 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~747 test was proposed in Ref. []. Refs. [3-7] tal over coonly used ways of describing a collision - e.g. investigation of tire ars or the crash energy approach. Vehicle crash investigation is an area of up-to-date technologies application. Refs. [8-] discuss usefulness of such developents as neural networs or fuzzy logic in the field of odeling of crash events. It is extreely iportant to assess what factors have an influence on the crash severity for an occupant. As in the case of a vehicle crash siulation, also here we can distinguish two ain ways of exaining the occupant behavior during an ipact. Ref. [3] focuses on finding the relationship between the car's daage and occupant injuries. On the other hand, Ref. [4] eploys FEM software to closely study the crash severity of particular body parts. In Refs. [5-8], basic atheatical odels are proposed to represent a collision. The ain part of this research is devoted to ethods of establishing paraeters of the vehicle crash odel and to real crash data investigation, e.g. creation of a Kelvin odel (spring and daper connected in parallel with ass) for a real experient, its analysis and validation. After odel's paraeters extraction a quic assessent of an occupant crash severity is done. Finally, the dynaic response of such a syste was siilar to the car's real behavior in the tie interval which corresponds to the collision's duration. Paraeters of this assebly (spring stiffness and daping coefficient) were obtained analytically with closed-for solutions according to Ref. [9]. In this paper, we present a process of iproving the accuracy of the vehicle crash odel. We start with siulation of the vehicle to pole ipact by using the Kelvin odel (spring and daper in parallel connected to ass). Afterwards, by filtering the crash pulse data, ore accurate response of the syste is obtained. Model establishent is done one ore tie. This allows us to copare what the crash odels are for both: raw and filtered data, and to decide which of the is ore suitable to represent vehicle to pole collision. In total, four different odels created for the filtered data are elaborated here and it is being assessed which of the gives the ost exact description of the car's behavior in the pole collision. The ain contribution of this paper is the evaluation of the proposed odeling ethodology results with the full-scale experiental data. When copared to the previous wor which concerns the siilar area of research [5], the current study presents ore detailed insight into vehicle localized ipact odeling. By the coparative analysis of different viscoelastic odels responses, it is decided which of the is the ost suitable to siulate vehicle-to-pole collision. To assess odel's fidelity, its structural properties and dynaic responses are exained. Fig.. Schee of the test collision [3]. Fig.. The car is undergoing deforation. Fig. 3. Kelvin odel.. Experiental setup In the experient conducted by UiA [4] the test vehicle, a standard Ford Fiesta. L 987 odel was subjected to a central ipact with a vertical, rigid cylinder at the initial ipact velocity v = 35 /h. Mass of the vehicle (together with the easuring equipent and duy) was 873 g. Experient's schee is shown in Fig.. Vehicle accelerations in three directions (longitudinal, lateral and vertical) together with the yaw rate at the center of gravity were easured. Using noral-speed and high-speed video caeras, the behavior of the obstruction and the test vehicle during the collision was recorded. Fig. shows one of the crash stages. 3. Raw data analysis - Kelvin odel According to Ref. [5], the Kelvin odel shown in Fig. 3 has been proposed to represent the vehicle to pole collision. Sybols used: - spring stiffness, c - daping coefficient, - ass, V - initial ipact velocity. Known paraeters of the odel are: = 873 g - ass V =.8 /s - initial ipact velocity. Paraeters which we obtain fro the crash pulse analysis (acceleration of the car in the x-direction - longitudinal) shown

3 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~ Table. Coparison between car s and Kelvin odel s responses - raw data. 6 4 Wideband data Filtered acceleration Paraeter Crash pulse analysis Kelvin odel Dynaic crush C [c] Tie of dynaic crush t [s] Acceleration [g]; velocity [/h]; crush [c] C=57c 8 t Acceleration =8s Velocity Crush 5 5 Tie [s] Fig. 4. Raw data analysis. Acceleration [g]; velocity [/h]; displaceent [c] Model acceleration 6 Model velocity Model displaceent Car acceleration 8 Car velocity Car displaceent 5 5 Tie [s] Fig. 5. Kelvin odel s response - raw data. in Fig. 4 are listed in Table. At the tie when the relative approach velocity is zero, the axiu dynaic crush occurs. The relative velocity in the rebound phase then increases negatively up to the final separation (or rebound) velocity, at which tie a vehicle rebounds fro an obstacle. The contact duration of the two asses includes both contact ties in deforation and restitution phases. When the relative acceleration becoes zero and relative separation velocity reaches its axiu recoverable value, separation of the two asses occurs. By following Ref. [9] (ethod of calculating daping factor ζ and natural frequency f is covered in Ref. [5]), spring stiffness and daping coefficient c of the Kelvin odel are deterined to be: = 4π f = 4 π (.9375 Hz) 873g = 9739 N/ c= 4π fζ= 4π.9375Hz. 873g = 33 N s/. Acceleration in x direction [g] Tie [s] Fig. 6. Butterworth 3 rd order filtering results. Aplitude x Wideband data Filtered acceleration Frequency [Hz] Frequency [Hz] Validation of the odel has been done in Matlab Siulin software - the response of the Kelvin odel with above estiated paraeters is shown in Fig. 5. Coparison of dynaic crush and tie of dynaic crush fro the crash pulse analysis and Kelvin odel response is done in Table. Rear. Since the raw data has been used above, the discrepancy between the real initial ipact velocity (which is V = 9.86 /s = 35 /h) and initial ipact velocity obtained fro the raw data analysis (which is V =.8 /s = 39 /h) is visible. Therefore, to eliinate inaccuracies in odeling caused by this velocity difference we need to filter the acceleration easureents. 4. Acceleration easureents filtering Digital filtering ethod has been used here [3]. Frequency response corridors for an appropriate channel class are specified in this standard. Since our goal is to analyze the crash pulse (i.e. integration for velocity and displaceent) we select the channel class CFC 8. Filter utilized by us was Butterworth 3rd order lowpass digital filter with cut-off frequency f N = 3 Hz. Coparison between the wideband data and data filtered with this ethod is shown in Fig. 6. In Fig. 7, the coparison in the frequency doain between the raw and filtered acceleration is presented. Since the scale is linear, we clearly see that the filtering helped us to get rid of the high frequency coponents of the crash pulse. This aes its analysis ore efficient and gives us results which better correspond to the reality than the ones obtained fro wideband data (velocity and displaceent). Aplitude x 4 Wideband data Filtered acceleration Fig. 7. Frequency analysis of crash pulses in linear scale (left - whole spectru, right - cut-off frequency region).

4 74 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~747 Table. Coparison between car s and Kelvin odel s responses - filtered data. Paraeter Crash pulse analysis Kelvin odel Dynaic crush C [c] Tie of dynaic crush t [s] Acceleration [g]; velocity [/h]; crush [c] Tie [s] Fig. 8. Filtered data analysis. Acceleration [g]; velocity [/h]; displaceent [c] 6 4 This has crucial influence on our further considerations because in order to develop a good odel, we need to have at our disposal real paraeters of the crash test (e.g. initial velocity). 5. Filtered data analysis 5. Kelvin odel Let us deterine what the axiu dynaic crush and the tie at which it occurs are for the filtered data. Paraeters which we obtain fro the crash pulse analysis (acceleration of the car in the x-direction - longitudinal) shown in Fig. 8 are listed in Table. Proceeding in the sae anner as in Section 3, we obtain the following paraeters of the Kelvin odel: = 4π f = 3445 N/ c = 4π fζ = 47 N s/. d c =5c t =76s Acceleration Velocity Crush Model acceleration Model velocity Model displaceent 4 Car acceleration Car velocity Car displaceent Tie [s] Fig. 9. Kelvin odel s response - filtered data. Fig.. Spring-ass odel. Kelvin odel response for those paraeters is shown in Fig. 9. Coparison between the odel and reality for the filtered data is done in Table. Filtering the data has iproved our calculations - we have obtained the real value of the initial velocity V = 9.86 /s = 35 /h. However, we observe a larger discrepancy between the dynaic crush fro the acceleration's integration and odel's prediction than for the raw data. This allows us to clai that since the ethod utilized in both of those cases reains the sae and accuracy of our calculations has increased because of the data filtering, the Kelvin odel is not suitable for odeling the ipact exained by us. For that reason we investigate a sipler odel which consists of spring and ass only. 5. Spring-ass odel The otion of this syste is a non-decayed oscillatory one (sinusoidal) because there is no daping in it [9]. This arrangeent is shown in Fig.. Sybols: - spring stiffness, - ass, a - absolute displaceent of ass. Let us introduce the following notation: V - initial barrier ipact velocity [/s] f - structural natural frequency [Hz]. Response of this syste is characterized by the following equations: α() t = Vωesin( ωet) () α() t = Vcos( ωet) () V α() t = sin( ωet) ω (3) e which represent deceleration, velocity and displaceent, respectively. Furtherore we define: V C = ω e (4) π t = ω (5) e ω e = (6)

5 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~ Table 3. Coparison between car s and spring-ass odel s responses - filtered data. Paraeter Crash pulse analysis Spring-ass odel Dynaic crush C [c] Tie of dynaic crush t [s] Acceleration [g]; velocity [/h]; displaceent [c] 6 4 Model acceleration Model velocity Model displaceent 4 Car acceleration Car velocity Car displaceent Tie [s] Fig.. Spring-ass odel s response. as axiu dynaic crush, tie of axiu dynaic crush and syste's circular natural frequency, respectively. To investigate what the paraeters C and t of such a odel are, first we need to find the spring stiffness. By substituting Eq. (6) to Eq. (4) and rearranging one gets: V =. (7) C Fro Fig. 8 it is obtained C =.5 = 5 c and V = 9.86 /s = 35 /h for filtered data. Therefore (9.86 / s) / = g = N (.5) π π π t = = = ωe N/ 873g =.83 s. Spring-ass odel's response for above spring stiffness (initial velocity and ass of the car reain the sae) is shown in Fig.. Let us copare what the dynaic crush and the tie at which it occurs are for the car and odel see Table 3. Results obtained in this step are good. The dynaic crush estiated by the spring-ass odel is exactly the sae as the reference dynaic crush of a real car. When it coes to the tie when it occurs, the difference between the odel and reality is less than %. This odel gives us good approxiation of the car's behavior during the crash. It is a particular case of a Kelvin odel in which daping has been set to zero as well as of a Maxwell odel in which daping goes to infinity. Fig.. Maxwell odel - designates zero-ass. 6. Maxwell odel - introduction The arrangeent in which spring and daper are connected in series to ass is called Maxwell odel - Fig.. To derive its equation of otion it is proposed to place sall ass ' between spring and daper. By doing this, the inertia effect which occurs for the spring and daper is neglected and the syste becoes third order differential equation which can be solved explicitly [9]. According to Fig. we define d and d' as absolute displaceent of ass and absolute displaceent of ass ', respectively. We establish the following equations of otion (EOM): d = c( d d') (8) d ' ' = cd ( d') d'. (9) By differentiating Eq. (8) and Eq. (9) w.r.t. tie and setting ' = we obtain: d = c( d d') () = cd ( d') d'. () We su up both sides of Eqs. () and () and rearrange: d' = d. () We substitute Eq. () into Eq. (8) and finally obtain the EOM found below: d+ d+ d =. (3) c Therefore, characteristic equation of the Maxwell odel is: ss [ + s ]. c + = (4) In this syste, the rebound of the ass depends on the sign of discriinant Δ of the quadratic equation in bracets. For positive Δ there is no rebound, i.e.: > 4. c

6 74 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~747 In this case, roots of the characteristic equations (Eq. (4)) are, respectively: s = s = a+ b s = a b where: a = c b =. c On the other hand, for negative Δ the rebound occurs when: v ad d = b d = d. However, in a Maxwell odel, the ass ay not rebound fro the obstacle. It eans that its displaceent increases with tie to an asyptotic value. The paraeter, which deterines whether the rebound will occur or not, is daping coefficient. When it is less than a liiting one (naed transition daping coefficient c*), the ass will be constantly approaching an obstacle, whereas when it is higher, there will exist a dynaic crush at a finite tie. Another boundary situation is for daping coefficient c =. Then the Maxwell odel degenerates into spring-ass syste. To deterine the value of transition daping coefficient we assue that c =, or equivalently < 4. c c = * In this case, roots of the characteristic equation (Eq. (4)) are, respectively: s = s = a+ ib s = a ib where: a = c b = c. Since this case is of our greater interest than the previous one (due to the fact that in the experient rebound occurred) we will describe in details its response. Displaceent of a ass is given by the forula: α = de + e [ dsin( bt) + d cos( bt)]. (5) st at Initial conditions (t = ) are: α = α = v α =. where v is the initial ipact velocity. Constants are: av d = a + b and * c =. (6) Indeed, for c < c * we have Δ > - it eans no dynaic crush at a finite tie. We are able to assess what the inial daping should be, which we add to the siple spring-ass odel entioned above, which will produce the dynaic crush not extended in an infinite period of tie. According to Eq. (6), for the odel and crash test being analyzed in Section 5., we calculate the transition daping coefficient: * N/ 873g c = = 877 N s/. For every daping greater than this value, the Maxwell odel fored fro the spring-ass odel fro Section 5., will give us the response ore and ore siilar to the springass odel characteristics presented in Fig., as it is shown in Fig. 3. It is noting that the final displaceent (or asyptotic value - for transition daping coefficient) achieved by the ass in this odel is characterized by the equation (V - initial ipact velocity, - ass, c - daping coefficient): crush V c =. (7) This syste is appropriate for siulating soft ipacts or offset ipacts because the tie of dynaic crush is longer than for Kelvin odel. We assue the sae paraeters for

7 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~ Displaceent [] c * c *.4 4c * Infinite daping Tie [s] Fig. 3. Maxwell odel responses for different values of daping. 7. Maxwell odel analysis When it coes to Maxwell odel, we will discuss just two cases for which Δ <, i.e. when the rebound occurs, because that is what happens during the experient. We are going to start with the siplification of this situation, in which daping coefficient of this odel has a liiting, transitional value. Then we proceed to the full Maxwell odel's analysis. 7. Maxwell odel with transition daping coefficient This is the particular case of a Maxwell odel in which ass' displaceent reaches an asyptotic value given by Eq. (7). For * c = paraeters of Eq. (5) degenerate into: Displaceent [] Maxwell odel Kelvin odel a = ω b = v d = b d = v ω d = v ω.5 Kelvin t =.9s Maxwell t =.8s where Tie [s] Fig. 4. Maxwell and Kelvin odels responses coparison. both odels, e.g.: = N/, c = 5 N-s/, = 5 g, v = /s. In Fig. 4, it is seen that for the Maxwell odel the dynaic crush occurs later than for the Kelvin odel. This is an analog situation to the real crash: in a vehicle-torigid barrier collision (Kelvin odel) the whole ipact energy is being consued faster, therefore the crash is ore dynaic than the vehicle-to-pole collision (Maxwell odel) - under the assuption that we copare the sae cars with the sae initial ipact velocities - as in the exaple above. It is noting that we do not investigate here the agnitude of the displaceent of both odels - as we can see for the sae paraeters it is higher for the Maxwell odel. Above exaple just illustrates the dynaic responses of those two systes and in order to apply those two odels to the real crash one needs to assess what spring stiffness and daping coefficient of both of the are separately. ω =. We tae advantage of the following trigonoetric relationships: sin( bt) li = t b b licos( bt) =. b Finally we coe up with the following equation of ass' displaceent: v t α = [ ( ωt + ) e ω ]. (8) ω To establish the paraeters of the Maxwell odel (spring stiffness and daping coefficient c) we just substitute to Eq. (8) values of initial ipact velocity v, axiu dynaic crush α and tie of axiu dynaic crush t taen fro the acceleration easureents analysis shown in Fig. 8 - we obtain ω = 37.5 rad/s. Knowing circular natural frequency ω and ass of the whole vehicle = 873 g, we calculate spring stiffness and transition daping coefficient c*: = ω = = 8966 N/ * c = = = 6377 N s/ Response of the odel with above coputed paraeters

8 744 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~747 6 Acceleration [g]; velocity [/h]; displaceent [c] 4 Model acceleration Model velocity Model displaceent 4 Car acceleration Car velocity Car displaceent Tie [s] Displaceent [] Experient Fitting.5..5 Tie [s] Fig. 5. Maxwell odel s (transition daping coefficient) response. and initial ipact velocity v = 9.86 /s = 35 /h is shown in Fig. 5. As we can see the value of axiu dynaic crush is the sae as the one obtained fro the experient's data analysis (C =.5 ) and tie when it occurs is uch longer - approxiately t =. s (copared to experient's t =.76 s). 7. Maxwell odel - rebound Response of the Maxwell odel is described by Eq. (5). Having the car's displaceent curve fro the experient we can establish paraeters of the odel (spring stiffness and daping coefficient c) just by fitting the curve defined by Eq. (5) to that real graph. However paraeters which we obtain by fitting Eq. (5) are: a, b, d, d and d. Since d and d (we do not discuss d separately because d = -d ) are functions of v as well, it is not guaranteed that the odel's paraeters which we obtained would be correct - in another words, v wouldn't be fixed if we fit Eq. (5) to the experient's displaceent. Therefore we express Eq. (5) only in ters of a and b (which are just functions of, c and ass = 873 g) and set initial ipact velocity to v = 9.86 /s. The equation which we obtain has the following for: av α = + a + b av v at a b av e + sin( bt) + cos( bt). b a + b (9) Fitting Eq. (9) to the experient's results has been done in Matlab Curve Fitting Toolbox and is shown in Fig. 6. Fitting Eq. (9) not Eq. (5) resulted in loss of approxiation's accuracy but on the other hand, we are sure that the initial ipact velocity has the correct value. Fro the above operation we obtain paraeters a and b of Eq. (9) which are equal to: a = = 4.79 c s Fig. 6. Fitting the Maxwell odel's response to the real experient's displaceent. Acceleration [g]; velocity [/h]; displaceent [c] 6 4 Model acceleration Model velocity Model displaceent 4 Car acceleration Car velocity Car displaceent Tie [s] Fig. 7. Coplete Maxwell odel s response. b = =.6. c s Now we have all we need to calculate daping coefficient c and spring stiffness of the Maxwell odel, respectively: a ( + b) c= = 9546 N s/ a = ac = 5787 N/. Response of the odel is shown in Fig. 7. As we can see the value of axiu dynaic crush is exactly the sae as the one obtained fro the experient's data analysis (C = 5 c) and tie when it occurs is longer - t = 4 s (copared to the experient's t = 76 s). However, as it is going to be shown in the following Section, the overall response of the Maxwell odel is the ost siilar to the car's behavior during collision with a pole. 8. Models coparison To represent vehicle to pole collision we established in total four odels here (spring-ass odel, Kelvin odel, Maxwell odel with transition daping coefficient and coplete Maxwell odel). Let us copare their responses with the car's

9 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~ Displaceent [c] Real car Kelvin odel Spring ass odel Maxwell odel (transition daping) Maxwell odel 5 5 Tie [s] Fig. 8. Models responses coparison. behavior during the experient analyzed by us - see Fig. 8. Characteristics which the best represents the overall car's behavior during the crash period belongs to the Maxwell odel. Although Kelvin and spring-ass odels give good approxiation in the beginning of the crash (up to the tie of axiu dynaic crush), they copletely fail when it coes to the crash representation after the rebound. Maxwell odel with transition daping coefficient shows correctly just the axiu dynaic crush, not its tie at all. Therefore the Maxwell odel gives the best overall outcoe - there is no difference in axiu displaceent and about 7% of divergence for tie of axiu dynaic crush coparing to the reality. And the entire shape of the Maxwell odel's response resebles closely the real car's crush. 9. Conclusion and future wors In this paper, we studied a process of iproving the accuracy of the vehicle crash odel. First, we siulated the vehicle under a pole ipact by using the Kelvin odel. Afterwards, by filtering the crash pulse data, ore accurate response of the syste was obtained. Model establishent was done one ore tie. Finally, we copared the crash odels and it was concluded which of the is ore suitable to represent vehicle to pole collision. The obtained results indicate that the Kelvin odel is not appropriate for siulation of the collision which we deal with. Based on Section 6, for the data prepared in the proper way, we establish a proper odel. Results obtained fro studying Maxwell odel provided us with satisfactory results. Coparative analysis of the odel's and real car's responses turned out to be appropriate. Therefore if one wants to siulate a vehicle to pole collision it is advisable to use Maxwell odel. It is desirable to verify whether the other viscoelastic odels which were not discussed in this paper are capable of vehicle crash siulation. In particular, so called hybrid odels (systes coposed of two springs, one daper, and a ass) ay be proising for this application. Furtherore, a twoass-spring-daper odel can be used to represent interactions between fore- and aft-frae of a vehicle. On top of that, it is advisable to exaine ethods for nonlinear syste paraeters identification. Since all the odels presented in the current study are luped paraeter ones which are valid only for the data which were used for their creation, they cannot be used to siulate e.g. a high-speed vehicle collision. However, the capabilities of atheatical odels with nonlinear paraeters (stiffness and daping) to siulate a variety of crash events are required to be assessed. Noenclature : Spring stiffness c : Daping coefficient : Mass V ; V : Initial ipact velocity ζ : Daping factor f : Structural natural frequency C : Maxiu dynaic crush t : Tie of axiu dynaic crush f N : Cut-off frequency a; d : Absolute displaceent of ass α : Model displaceent ω e ; ω : Circular natural frequency : Zero-ass d : Absolute displaceent of ass c * : Transition daping coefficient Δ : Discriinant References [] M. Borovinse, M. Vesenja, M. Ulbin and Z. Ren, Siulation of crash tests for high containent levels of road safety barriers, Engineering Failure Analysis, 4 (8) (7) [] R. Harb, E. Radwan, X. Yan and M. Abdel-Aty, Light truc vehicles (LTVs) contribution to rear-end collisions, Accident Analysis & Prevention, 39 (5) (7) [3] A. Soica and S. Lache, Theoretical and experiental approaches to otor vehicle: pedestrian collision, 3rd WSEAS International Conference on Applied and Theoretcial Mechanics, Spain, Deceber (7). [4] O. Klyavin, A. Michailov and A. Borovov, Finite eleent odeling of the crash-tests for energy absorbing lighting coluns, ENOC-8, Saint Petersburg, Russia, June (8). [5] C. -H. Lin, Modeling and siulation of van for side ipact sensing tests, General Motors R&D Center, USA, Paper Nuber 7-6 (7). [6] A. Bižal, K. Jernej, R. Uroš and F. Matija, Nuerical siulation of crash test for the vehicle student roadster, FISITA 8 (8). [7] R. J. Yang, L. Tseng, L. Nagy, and J. Cheng, Feasibility study of crash optiization, advances in design autoation, Proceedings of the 994 ASME Design Technical Conference, th Design Autoation Conference, Minneapolis, Minnesota, USA, 69 () (994) [8] J. A. Neptune and J. E. Flynn, A ethod for deterining

10 746 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~747 crush stiffness coefficients fro offset frontal and side crash tests, SAE Paper 984 (998). [9] A. Deb and K. C. Srinivas, Developent of a new lupedparaeter odel for vehicle side-ipact safety siulation, Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Autoobile Engineering, () (8) [] P. Jonsén, E. Isasson, K. G. Sundin and M. Oldenburg, Identification of luped paraeter autootive crash odels for buper syste developent, International Journal of Crashworthiness, 4 (6) (9) [] M. S. Varat and S. E. Husher: Crash pulse odeling for vehicle safety research, 8th ESV Paper (). [] H. R. Karii and K. G. Robbersyr, Signal analysis and perforance evaluation of a vehicle crash test with a fixed safety barrier based on Haar wavelets, International Journal of Wavelets, Multiresoloution and Iage Processing, 9 () () [3] G. Šušteršič, I. Grabec and I. Prebil, Statistical odel of a vehicle-to-barrier collision, International Journal of Ipact Engineering, 34 () (7) [4] X. Y. Zhang, X. L. Jin and J. Shen, Virtual reconstruction of two types of traffic accident by the tire ars, Lecture Notes Coput. Sci. 48, (6) [5] D. Trusca, A. Soica, B. Benea, and S. Tarulescu, Coputer Siulation and Experiental Research of the Vehicle Ipact, WSEAS Transactions on Coputers, 8 () (9) [6] D. Vangi, Energy loss in vehicle to vehicle oblique ipact, International Journal of Ipact Engineering, 36 (3) (9) 5-5. [7] W. Pawlus, H. R. Karii and K. G. Robbersyr, Matheatical odeling of a vehicle crash test based on elastoplastic unloading scenarios of spring-ass odels, International Journal of Advanced Manufacturing Technology, DOI:.7/s x,. [8] T. Oar, A. Esandarian and N. Bedewi, Vehicle crash odelling using recurrent neural networs, Matheatical and Coputer Modelling, 8 (9) (998) 3-4. [9] I. A. Harati, A. Rovid, L. Szeidl and P. Varlai, Energy distribution odeling of car body deforation using LPV representations and fuzzy reasoning, WSEAS Transactions on Systes, 7 () (8) [] V. Giavotto, L. Puccinelli, M. Borri, A. Edelan and T. Heijer, Vehicle dynaics and crash dynaics with inicoputer, Coputers & Structures, 6 (-4) (983) [] W. Pawlus, J. E. Nielsen, H. R. Karii and K. G. Robbersyr. Coparative analysis of vehicle to pole collision odels established using analytical ethods and neural networs. The 5th IET International Syste Safety Conference, Manchester, UK, October (). [] W. Pawlus, H.R. Karii and K. G. Robbersyr, Analysis of vehicle to pole collision odels: analytical ethods and neural networs. International Journal of Control Theory and Applications, 3 () () [3] C. Conroy, G. T. Toinaga, S. Erwin, S. Pacyna, T. Vely, F. Kennedy, M. Sise and R. Coibra, The influence of vehicle daage on injury severity of drivers in head-on otor vehicle crashes, Accident Analysis & Prevention, 4 (4) (8) [4] Y. Niu, W. Shen and J. H. Stuhiller, Finite eleent odels of rib as an inhoogeneous bea structure under highspeed ipacts, Medical Engineering & Physics, 9 (7) (7) [5] W. Pawlus, J. E. Nielsen, H. R. Karii and K. G. Robbersyr, Matheatical odeling and analysis of a vehicle crash, 4th European Coputing Conference, Bucarest, Roania, April (). [6] W. Pawlus, J. E. Nielsen, H.R. Karii and K.G. Robbersyr, Developent of atheatical odels for analysis of a vehicle crash, WSEAS Transactions on Applied and Theoretical Mechanics, 5 () () [7] W. Pawlus, J. E. Nielsen, H. R. Karii and K. G. Robbersyr, Further results on atheatical odels of vehicle localized ipact, The 3rd International Syposiu on Systes and Control in Aeronautics and Astronautics, Harbin, China, June (). [8] W. Pawlus and J. E. Nielsen, Developent of atheatical odels for vehicle to pole collision, Shaer Publishing, Maastricht, The Netherlands (). [9] M. Huang, Vehicle Crash Mechanics, CRC Press, Boca Raton, USA (). [3] K. G. Robbersyr, Calibration test of a standard Ford Fiesta.L, odel year 987, according to NS-EN 767, Project Report 43/4, Gristad: Agder University College (4). [3] ISO 6487:, Road vehicles - easureent techniques in ipact tests instruentation. world phenoena. Witold Pawlus is a Research Assistant at the University of Agder in Norway. He received his B.Sc. in in Mechatronics fro AGH University of Science and Technology in Kraów, Poland. His research interests are within the area of nonlinear systes paraeters identification and atheatical odeling of real

11 W. Pawlus et al. / Journal of Mechanical Science and Technology 5 (7) () 737~ Haid Reza Karii is a Professor in Control Systes at the University of Agder in Norway. His research interests are in the areas of control theory with an ephasis on applications in engineering. Dr. Karii is a senior eber of IEEE and serves as a Chairan of the IEEE Chapter on Control Systes in Norway. He is also serving as an editorial board eber for soe international journals, such as Mechatronics, Journal of the Franlin Institute, etc. He is a eber of IEEE Technical Coittee on Systes with Uncertainty, IFAC Technical Coittees on Robust Control and on Autootive Control. Kjell G. Robbersyr is a Professor in Machine Design at both: the University of Agder and Hogsolen in Bergen in Norway. Machine design (coponent and syste design, product developent) and vehicle crash siulations (FEA) are his ain research interests. Fro 997 to 5 he was the leader of a scientific group woring in the area of full-scale crash testing, including e.g. perforance evaluation of safety barriers.

Mathematical modeling of a vehicle crash test based on elasto-plastic unloading scenarios of spring-mass models

Mathematical modeling of a vehicle crash test based on elasto-plastic unloading scenarios of spring-mass models Int J Adv Manuf Technol (211) 55:369 378 DOI 1.17/s17-1-356-x ORIGINAL ARTICLE Mathematical modeling of a vehicle crash test based on elasto-plastic unloading scenarios of spring-mass models Witold Pawlus

More information

Analysis of Impulsive Natural Phenomena through Finite Difference Methods A MATLAB Computational Project-Based Learning

Analysis of Impulsive Natural Phenomena through Finite Difference Methods A MATLAB Computational Project-Based Learning Analysis of Ipulsive Natural Phenoena through Finite Difference Methods A MATLAB Coputational Project-Based Learning Nicholas Kuia, Christopher Chariah, Mechatronics Engineering, Vaughn College of Aeronautics

More information

A recursive model for nonlinear spring-mass-damper estimation of a vehicle localized impact

A recursive model for nonlinear spring-mass-damper estimation of a vehicle localized impact A recursive model for nonlinear spring-mass-damper estimation of a vehicle localized impact HAMID REZA KARIMI hamid.r.karimi@uia.no WITOLD PAWLUS witolp9@student.uia.no KJELL G. ROBBERSMYR kjell.g.robbersmyr@uia.no

More information

ANALYTICAL INVESTIGATION AND PARAMETRIC STUDY OF LATERAL IMPACT BEHAVIOR OF PRESSURIZED PIPELINES AND INFLUENCE OF INTERNAL PRESSURE

ANALYTICAL INVESTIGATION AND PARAMETRIC STUDY OF LATERAL IMPACT BEHAVIOR OF PRESSURIZED PIPELINES AND INFLUENCE OF INTERNAL PRESSURE DRAFT Proceedings of the ASME 014 International Mechanical Engineering Congress & Exposition IMECE014 Noveber 14-0, 014, Montreal, Quebec, Canada IMECE014-36371 ANALYTICAL INVESTIGATION AND PARAMETRIC

More information

Chapter 1: Basics of Vibrations for Simple Mechanical Systems

Chapter 1: Basics of Vibrations for Simple Mechanical Systems Chapter 1: Basics of Vibrations for Siple Mechanical Systes Introduction: The fundaentals of Sound and Vibrations are part of the broader field of echanics, with strong connections to classical echanics,

More information

Numerical Studies of a Nonlinear Heat Equation with Square Root Reaction Term

Numerical Studies of a Nonlinear Heat Equation with Square Root Reaction Term Nuerical Studies of a Nonlinear Heat Equation with Square Root Reaction Ter Ron Bucire, 1 Karl McMurtry, 1 Ronald E. Micens 2 1 Matheatics Departent, Occidental College, Los Angeles, California 90041 2

More information

Mathematical Modelling of Car Crash Test

Mathematical Modelling of Car Crash Test REST Journal on Emerging trends in Modelling and Manufacturing Vol:3(3),2017 REST Publisher ISSN: 2455-4537 Website: www.restpublisher.com/journals/jemm Mathematical Modelling of Car Crash Test Abhinav

More information

Lecture #8-3 Oscillations, Simple Harmonic Motion

Lecture #8-3 Oscillations, Simple Harmonic Motion Lecture #8-3 Oscillations Siple Haronic Motion So far we have considered two basic types of otion: translation and rotation. But these are not the only two types of otion we can observe in every day life.

More information

Analysis of ground vibration transmission in high precision equipment by Frequency Based Substructuring

Analysis of ground vibration transmission in high precision equipment by Frequency Based Substructuring Analysis of ground vibration transission in high precision equipent by Frequency Based Substructuring G. van Schothorst 1, M.A. Boogaard 2, G.W. van der Poel 1, D.J. Rixen 2 1 Philips Innovation Services,

More information

DESIGN OF THE DIE PROFILE FOR THE INCREMENTAL RADIAL FORGING PROCESS *

DESIGN OF THE DIE PROFILE FOR THE INCREMENTAL RADIAL FORGING PROCESS * IJST, Transactions of Mechanical Engineering, Vol. 39, No. M1, pp 89-100 Printed in The Islaic Republic of Iran, 2015 Shira University DESIGN OF THE DIE PROFILE FOR THE INCREMENTAL RADIAL FORGING PROCESS

More information

DETECTION OF NONLINEARITY IN VIBRATIONAL SYSTEMS USING THE SECOND TIME DERIVATIVE OF ABSOLUTE ACCELERATION

DETECTION OF NONLINEARITY IN VIBRATIONAL SYSTEMS USING THE SECOND TIME DERIVATIVE OF ABSOLUTE ACCELERATION DETECTION OF NONLINEARITY IN VIBRATIONAL SYSTEMS USING THE SECOND TIME DERIVATIVE OF ABSOLUTE ACCELERATION Masaki WAKUI 1 and Jun IYAMA and Tsuyoshi KOYAMA 3 ABSTRACT This paper shows a criteria to detect

More information

ANALYSIS ON RESPONSE OF DYNAMIC SYSTEMS TO PULSE SEQUENCES EXCITATION

ANALYSIS ON RESPONSE OF DYNAMIC SYSTEMS TO PULSE SEQUENCES EXCITATION The 4 th World Conference on Earthquake Engineering October -7, 8, Beijing, China ANALYSIS ON RESPONSE OF DYNAMIC SYSTEMS TO PULSE SEQUENCES EXCITATION S. Li C.H. Zhai L.L. Xie Ph. D. Student, School of

More information

Chapter 11: Vibration Isolation of the Source [Part I]

Chapter 11: Vibration Isolation of the Source [Part I] Chapter : Vibration Isolation of the Source [Part I] Eaple 3.4 Consider the achine arrangeent illustrated in figure 3.. An electric otor is elastically ounted, by way of identical isolators, to a - thick

More information

NUMERICAL MODELLING OF THE TYRE/ROAD CONTACT

NUMERICAL MODELLING OF THE TYRE/ROAD CONTACT NUMERICAL MODELLING OF THE TYRE/ROAD CONTACT PACS REFERENCE: 43.5.LJ Krister Larsson Departent of Applied Acoustics Chalers University of Technology SE-412 96 Sweden Tel: +46 ()31 772 22 Fax: +46 ()31

More information

Chapter 2: Introduction to Damping in Free and Forced Vibrations

Chapter 2: Introduction to Damping in Free and Forced Vibrations Chapter 2: Introduction to Daping in Free and Forced Vibrations This chapter ainly deals with the effect of daping in two conditions like free and forced excitation of echanical systes. Daping plays an

More information

SEISMIC FRAGILITY ANALYSIS

SEISMIC FRAGILITY ANALYSIS 9 th ASCE Specialty Conference on Probabilistic Mechanics and Structural Reliability PMC24 SEISMIC FRAGILITY ANALYSIS C. Kafali, Student M. ASCE Cornell University, Ithaca, NY 483 ck22@cornell.edu M. Grigoriu,

More information

Accuracy of the Scaling Law for Experimental Natural Frequencies of Rectangular Thin Plates

Accuracy of the Scaling Law for Experimental Natural Frequencies of Rectangular Thin Plates The 9th Conference of Mechanical Engineering Network of Thailand 9- October 005, Phuket, Thailand Accuracy of the caling Law for Experiental Natural Frequencies of Rectangular Thin Plates Anawat Na songkhla

More information

SEISMIC SAFETY OF BRIDGE CRANE STEEL STRUCTURES OPERATING IN NPP

SEISMIC SAFETY OF BRIDGE CRANE STEEL STRUCTURES OPERATING IN NPP SEISMIC SAFETY OF BRIDGE CRANE STEEL STRUCTURES OPERATING IN NPP Kalin RADLOV*, Vesko PANOV** *University of Architecture, Civil Engineering and Geodesy Sofia, Bulgaria **Technical University Sofia, Bulgaria

More information

Monitoring and system identification of suspension bridges: An alternative approach

Monitoring and system identification of suspension bridges: An alternative approach Monitoring and syste identification of suspension bridges: An alternative approach Erdal Şafak Boğaziçi University, Kandilli Observatory and Earthquake Reseach Institute, Istanbul, Turkey Abstract This

More information

REDUCTION OF FINITE ELEMENT MODELS BY PARAMETER IDENTIFICATION

REDUCTION OF FINITE ELEMENT MODELS BY PARAMETER IDENTIFICATION ISSN 139 14X INFORMATION TECHNOLOGY AND CONTROL, 008, Vol.37, No.3 REDUCTION OF FINITE ELEMENT MODELS BY PARAMETER IDENTIFICATION Riantas Barauskas, Vidantas Riavičius Departent of Syste Analysis, Kaunas

More information

Extension of CSRSM for the Parametric Study of the Face Stability of Pressurized Tunnels

Extension of CSRSM for the Parametric Study of the Face Stability of Pressurized Tunnels Extension of CSRSM for the Paraetric Study of the Face Stability of Pressurized Tunnels Guilhe Mollon 1, Daniel Dias 2, and Abdul-Haid Soubra 3, M.ASCE 1 LGCIE, INSA Lyon, Université de Lyon, Doaine scientifique

More information

Qualitative Modelling of Time Series Using Self-Organizing Maps: Application to Animal Science

Qualitative Modelling of Time Series Using Self-Organizing Maps: Application to Animal Science Proceedings of the 6th WSEAS International Conference on Applied Coputer Science, Tenerife, Canary Islands, Spain, Deceber 16-18, 2006 183 Qualitative Modelling of Tie Series Using Self-Organizing Maps:

More information

ACTIVE VIBRATION CONTROL FOR STRUCTURE HAVING NON- LINEAR BEHAVIOR UNDER EARTHQUAKE EXCITATION

ACTIVE VIBRATION CONTROL FOR STRUCTURE HAVING NON- LINEAR BEHAVIOR UNDER EARTHQUAKE EXCITATION International onference on Earthquae Engineering and Disaster itigation, Jaarta, April 14-15, 8 ATIVE VIBRATION ONTROL FOR TRUTURE HAVING NON- LINEAR BEHAVIOR UNDER EARTHQUAE EXITATION Herlien D. etio

More information

16.30/31 September 24, 2010 Prof. J. P. How and Prof. E. Frazzoli Due: October 15, 2010 T.A. B. Luders /31 Lab #1

16.30/31 September 24, 2010 Prof. J. P. How and Prof. E. Frazzoli Due: October 15, 2010 T.A. B. Luders /31 Lab #1 16.30/31 Septeber 24, 2010 Prof. J. P. How and Prof. E. Frazzoli Due: October 15, 2010 T.A. B. Luders 16.30/31 Lab #1 1 Introduction The Quanser helicopter is a echanical device that eulates the flight

More information

An Approximate Model for the Theoretical Prediction of the Velocity Increase in the Intermediate Ballistics Period

An Approximate Model for the Theoretical Prediction of the Velocity Increase in the Intermediate Ballistics Period An Approxiate Model for the Theoretical Prediction of the Velocity... 77 Central European Journal of Energetic Materials, 205, 2(), 77-88 ISSN 2353-843 An Approxiate Model for the Theoretical Prediction

More information

On the Mutual Coefficient of Restitution in Two Car Collinear Collisions

On the Mutual Coefficient of Restitution in Two Car Collinear Collisions /4/006 physics/06068 On the Mutual Coefficient of Restitution in Two Car Collinear Collisions Milan Batista University of Ljubljana, Faculty of Maritie Studies and Transportation Pot poorscakov 4, Slovenia,

More information

Dynamic analysis of frames with viscoelastic dampers: a comparison of damper models

Dynamic analysis of frames with viscoelastic dampers: a comparison of damper models Structural Engineering and Mechanics, Vol. 41, No. 1 (2012) 113-137 113 Dynaic analysis of fraes with viscoelastic dapers: a coparison of daper odels R. Lewandowski*, A. Bartkowiak a and H. Maciejewski

More information

T m. Fapplied. Thur Oct 29. ω = 2πf f = (ω/2π) T = 1/f. k m. ω =

T m. Fapplied. Thur Oct 29. ω = 2πf f = (ω/2π) T = 1/f. k m. ω = Thur Oct 9 Assignent 10 Mass-Spring Kineatics (x, v, a, t) Dynaics (F,, a) Tie dependence Energy Pendulu Daping and Resonances x Acos( ωt) = v = Aω sin( ωt) a = Aω cos( ωt) ω = spring k f spring = 1 k

More information

Symbolic Analysis as Universal Tool for Deriving Properties of Non-linear Algorithms Case study of EM Algorithm

Symbolic Analysis as Universal Tool for Deriving Properties of Non-linear Algorithms Case study of EM Algorithm Acta Polytechnica Hungarica Vol., No., 04 Sybolic Analysis as Universal Tool for Deriving Properties of Non-linear Algoriths Case study of EM Algorith Vladiir Mladenović, Miroslav Lutovac, Dana Porrat

More information

IN modern society that various systems have become more

IN modern society that various systems have become more Developent of Reliability Function in -Coponent Standby Redundant Syste with Priority Based on Maxiu Entropy Principle Ryosuke Hirata, Ikuo Arizono, Ryosuke Toohiro, Satoshi Oigawa, and Yasuhiko Takeoto

More information

Vibration Characteristics of Cardboard Inserts in Shells

Vibration Characteristics of Cardboard Inserts in Shells 2003-01-1489 Vibration Characteristics of Cardboard Inserts in Shells Martin G. Foulkes and Jaes P. De Clerck General Motors Corporation Raendra Singh he Ohio State University Copyright 2003 SAE International

More information

USEFUL HINTS FOR SOLVING PHYSICS OLYMPIAD PROBLEMS. By: Ian Blokland, Augustana Campus, University of Alberta

USEFUL HINTS FOR SOLVING PHYSICS OLYMPIAD PROBLEMS. By: Ian Blokland, Augustana Campus, University of Alberta 1 USEFUL HINTS FOR SOLVING PHYSICS OLYMPIAD PROBLEMS By: Ian Bloland, Augustana Capus, University of Alberta For: Physics Olypiad Weeend, April 6, 008, UofA Introduction: Physicists often attept to solve

More information

Optical Properties of Plasmas of High-Z Elements

Optical Properties of Plasmas of High-Z Elements Forschungszentru Karlsruhe Techni und Uwelt Wissenschaftlishe Berichte FZK Optical Properties of Plasas of High-Z Eleents V.Tolach 1, G.Miloshevsy 1, H.Würz Project Kernfusion 1 Heat and Mass Transfer

More information

Generalized Rayleigh Wave Dispersion in a Covered Half-space Made of Viscoelastic Materials

Generalized Rayleigh Wave Dispersion in a Covered Half-space Made of Viscoelastic Materials Copyright 7 Tech Science Press CMC vol.53 no.4 pp.37-34 7 Generalized Rayleigh Wave Dispersion in a Covered Half-space Made of Viscoelastic Materials S.D. Akbarov and M. Negin 3 Abstract: Dispersion of

More information

PY241 Solutions Set 9 (Dated: November 7, 2002)

PY241 Solutions Set 9 (Dated: November 7, 2002) PY241 Solutions Set 9 (Dated: Noveber 7, 2002) 9-9 At what displaceent of an object undergoing siple haronic otion is the agnitude greatest for the... (a) velocity? The velocity is greatest at x = 0, the

More information

821. Study on analysis method for deepwater TTR coupled vibration of parameter vibration and vortex-induced vibration

821. Study on analysis method for deepwater TTR coupled vibration of parameter vibration and vortex-induced vibration 81. Study on analysis ethod for deepwater TTR coupled vibration of paraeter vibration and vortex-induced vibration Wu Xue-Min 1, Huang Wei-Ping Shandong Key aboratory of Ocean Engineering, Ocean University

More information

Physics 2107 Oscillations using Springs Experiment 2

Physics 2107 Oscillations using Springs Experiment 2 PY07 Oscillations using Springs Experient Physics 07 Oscillations using Springs Experient Prelab Read the following bacground/setup and ensure you are failiar with the concepts and theory required for

More information

Name: Partner(s): Date: Angular Momentum

Name: Partner(s): Date: Angular Momentum Nae: Partner(s): Date: Angular Moentu 1. Purpose: In this lab, you will use the principle of conservation of angular oentu to easure the oent of inertia of various objects. Additionally, you develop a

More information

AiMT Advances in Military Technology

AiMT Advances in Military Technology AiT Advances in ilitary Technology Vol. 14, No. 1 (2019), pp. 47-57 ISSN 1802-2308, eissn 2533-4123 DOI 10.3849/ait.01247 odelling issile Flight Characteristics by Estiating ass and Ballistic Paraeters

More information

PHY 171. Lecture 14. (February 16, 2012)

PHY 171. Lecture 14. (February 16, 2012) PHY 171 Lecture 14 (February 16, 212) In the last lecture, we looked at a quantitative connection between acroscopic and icroscopic quantities by deriving an expression for pressure based on the assuptions

More information

TOPIC E: OSCILLATIONS SPRING 2018

TOPIC E: OSCILLATIONS SPRING 2018 TOPIC E: OSCILLATIONS SPRING 018 1. Introduction 1.1 Overview 1. Degrees of freedo 1.3 Siple haronic otion. Undaped free oscillation.1 Generalised ass-spring syste: siple haronic otion. Natural frequency

More information

Determining a Function for the Damping Coefficient of a laminated Stack

Determining a Function for the Damping Coefficient of a laminated Stack DOI: 10.435/UB.OVGU-017-093 TECHNISCHE MECHANIK, 37, -5, (017), 161 170 subitted: June 9, 017 Deterining a Function for the Daping Coefficient of a lainated Stack C. Zahalka, K. Ellerann The design of

More information

This is a repository copy of Analytical optimisation of electromagnetic design of a linear (tubular) switched reluctance motor.

This is a repository copy of Analytical optimisation of electromagnetic design of a linear (tubular) switched reluctance motor. This is a repository copy of Analytical optiisation of electroagnetic design of a linear (tubular) switched reluctance otor. White Rose Research Online URL for this paper: http://eprints.whiterose.ac.uk/907/

More information

An Inverse Interpolation Method Utilizing In-Flight Strain Measurements for Determining Loads and Structural Response of Aerospace Vehicles

An Inverse Interpolation Method Utilizing In-Flight Strain Measurements for Determining Loads and Structural Response of Aerospace Vehicles An Inverse Interpolation Method Utilizing In-Flight Strain Measureents for Deterining Loads and Structural Response of Aerospace Vehicles S. Shkarayev and R. Krashantisa University of Arizona, Tucson,

More information

Data-Driven Imaging in Anisotropic Media

Data-Driven Imaging in Anisotropic Media 18 th World Conference on Non destructive Testing, 16- April 1, Durban, South Africa Data-Driven Iaging in Anisotropic Media Arno VOLKER 1 and Alan HUNTER 1 TNO Stieltjesweg 1, 6 AD, Delft, The Netherlands

More information

MSEC MODELING OF DEGRADATION PROCESSES TO OBTAIN AN OPTIMAL SOLUTION FOR MAINTENANCE AND PERFORMANCE

MSEC MODELING OF DEGRADATION PROCESSES TO OBTAIN AN OPTIMAL SOLUTION FOR MAINTENANCE AND PERFORMANCE Proceeding of the ASME 9 International Manufacturing Science and Engineering Conference MSEC9 October 4-7, 9, West Lafayette, Indiana, USA MSEC9-8466 MODELING OF DEGRADATION PROCESSES TO OBTAIN AN OPTIMAL

More information

Research and Experiments on Electromagnetic Field Induced by Two. Coaxial Solenoid Coils of Axially Mag-lev Driving Needle

Research and Experiments on Electromagnetic Field Induced by Two. Coaxial Solenoid Coils of Axially Mag-lev Driving Needle 3rd International Conference on Mechatronics and Inforation Technology (ICMIT 16) Research and Experients on Electroagnetic Field Induced by Two Coaxial Solenoid Coils of Axially Mag-lev Driving Needle

More information

Use of PSO in Parameter Estimation of Robot Dynamics; Part One: No Need for Parameterization

Use of PSO in Parameter Estimation of Robot Dynamics; Part One: No Need for Parameterization Use of PSO in Paraeter Estiation of Robot Dynaics; Part One: No Need for Paraeterization Hossein Jahandideh, Mehrzad Navar Abstract Offline procedures for estiating paraeters of robot dynaics are practically

More information

ANALYSIS OF HALL-EFFECT THRUSTERS AND ION ENGINES FOR EARTH-TO-MOON TRANSFER

ANALYSIS OF HALL-EFFECT THRUSTERS AND ION ENGINES FOR EARTH-TO-MOON TRANSFER IEPC 003-0034 ANALYSIS OF HALL-EFFECT THRUSTERS AND ION ENGINES FOR EARTH-TO-MOON TRANSFER A. Bober, M. Guelan Asher Space Research Institute, Technion-Israel Institute of Technology, 3000 Haifa, Israel

More information

Imbalance Estimation for Speed-Varying Rigid Rotors Using Time-Varying Observer

Imbalance Estimation for Speed-Varying Rigid Rotors Using Time-Varying Observer Shiyu Zhou e-ail: zhous@uich.edu Jianjun Shi 1 e-ail: shihang@uich.edu Departent of Industrial and Operations Engineering, The University of Michigan, Ann Arbor, MI 48109 Ibalance Estiation for Speed-Varying

More information

ma x = -bv x + F rod.

ma x = -bv x + F rod. Notes on Dynaical Systes Dynaics is the study of change. The priary ingredients of a dynaical syste are its state and its rule of change (also soeties called the dynaic). Dynaical systes can be continuous

More information

Question 1. [14 Marks]

Question 1. [14 Marks] 6 Question 1. [14 Marks] R r T! A string is attached to the dru (radius r) of a spool (radius R) as shown in side and end views here. (A spool is device for storing string, thread etc.) A tension T is

More information

Torsion Experiment. Encoder #3 ( 3 ) Third encoder/disk for Model 205a only. Figure 1: ECP Torsion Experiment

Torsion Experiment. Encoder #3 ( 3 ) Third encoder/disk for Model 205a only. Figure 1: ECP Torsion Experiment Torsion Experient Introduction For the Torsion lab, there are two required experients to perfor and one extra credit assignent at the end. In experient 1, the syste paraeters need to be identified so that

More information

Motion Analysis of Euler s Disk

Motion Analysis of Euler s Disk Motion Analysis of Euler s Disk Katsuhiko Yaada Osaka University) Euler s Disk is a nae of a scientific toy and its otion is the sae as a spinning coin. In this study, a siple atheatical odel is proposed

More information

Support Vector Machine Classification of Uncertain and Imbalanced data using Robust Optimization

Support Vector Machine Classification of Uncertain and Imbalanced data using Robust Optimization Recent Researches in Coputer Science Support Vector Machine Classification of Uncertain and Ibalanced data using Robust Optiization RAGHAV PAT, THEODORE B. TRAFALIS, KASH BARKER School of Industrial Engineering

More information

Scattering and bound states

Scattering and bound states Chapter Scattering and bound states In this chapter we give a review of quantu-echanical scattering theory. We focus on the relation between the scattering aplitude of a potential and its bound states

More information

9 HOOKE S LAW AND SIMPLE HARMONIC MOTION

9 HOOKE S LAW AND SIMPLE HARMONIC MOTION Experient 9 HOOKE S LAW AND SIMPLE HARMONIC MOTION Objectives 1. Verify Hoo s law,. Measure the force constant of a spring, and 3. Measure the period of oscillation of a spring-ass syste and copare it

More information

Ph 20.3 Numerical Solution of Ordinary Differential Equations

Ph 20.3 Numerical Solution of Ordinary Differential Equations Ph 20.3 Nuerical Solution of Ordinary Differential Equations Due: Week 5 -v20170314- This Assignent So far, your assignents have tried to failiarize you with the hardware and software in the Physics Coputing

More information

A Simulation Study for Practical Control of a Quadrotor

A Simulation Study for Practical Control of a Quadrotor A Siulation Study for Practical Control of a Quadrotor Jeongho Noh* and Yongkyu Song** *Graduate student, Ph.D. progra, ** Ph.D., Professor Departent of Aerospace and Mechanical Engineering, Korea Aerospace

More information

Kernel Methods and Support Vector Machines

Kernel Methods and Support Vector Machines Intelligent Systes: Reasoning and Recognition Jaes L. Crowley ENSIAG 2 / osig 1 Second Seester 2012/2013 Lesson 20 2 ay 2013 Kernel ethods and Support Vector achines Contents Kernel Functions...2 Quadratic

More information

Using a De-Convolution Window for Operating Modal Analysis

Using a De-Convolution Window for Operating Modal Analysis Using a De-Convolution Window for Operating Modal Analysis Brian Schwarz Vibrant Technology, Inc. Scotts Valley, CA Mark Richardson Vibrant Technology, Inc. Scotts Valley, CA Abstract Operating Modal Analysis

More information

A DESIGN GUIDE OF DOUBLE-LAYER CELLULAR CLADDINGS FOR BLAST ALLEVIATION

A DESIGN GUIDE OF DOUBLE-LAYER CELLULAR CLADDINGS FOR BLAST ALLEVIATION International Journal of Aerospace and Lightweight Structures Vol. 3, No. 1 (2013) 109 133 c Research Publishing Services DOI: 10.3850/S201042862013000550 A DESIGN GUIDE OF DOUBLE-LAYER CELLULAR CLADDINGS

More information

Periodic Motion is everywhere

Periodic Motion is everywhere Lecture 19 Goals: Chapter 14 Interrelate the physics and atheatics of oscillations. Draw and interpret oscillatory graphs. Learn the concepts of phase and phase constant. Understand and use energy conservation

More information

Supervised assessment: Modelling and problem-solving task

Supervised assessment: Modelling and problem-solving task Matheatics C 2008 Saple assessent instruent and indicative student response Supervised assessent: Modelling and proble-solving tas This saple is intended to infor the design of assessent instruents in

More information

Reducing Vibration and Providing Robustness with Multi-Input Shapers

Reducing Vibration and Providing Robustness with Multi-Input Shapers 29 Aerican Control Conference Hyatt Regency Riverfront, St. Louis, MO, USA June -2, 29 WeA6.4 Reducing Vibration and Providing Robustness with Multi-Input Shapers Joshua Vaughan and Willia Singhose Abstract

More information

Analysis and Implementation of a Hardware-in-the-Loop Simulation

Analysis and Implementation of a Hardware-in-the-Loop Simulation DINAME 27 - Proceedings of the XVII International Syposiu on Dynaic Probles of Mechanics A. T. Fleury, D. A. Rade, P. R. G. Kurka (Editors), ABCM, São Sebastião, SP, Brail, March 5-, 27 Analysis and Ipleentation

More information

UNCERTAINTIES IN THE APPLICATION OF ATMOSPHERIC AND ALTITUDE CORRECTIONS AS RECOMMENDED IN IEC STANDARDS

UNCERTAINTIES IN THE APPLICATION OF ATMOSPHERIC AND ALTITUDE CORRECTIONS AS RECOMMENDED IN IEC STANDARDS Paper Published on the16th International Syposiu on High Voltage Engineering, Cape Town, South Africa, 2009 UNCERTAINTIES IN THE APPLICATION OF ATMOSPHERIC AND ALTITUDE CORRECTIONS AS RECOMMENDED IN IEC

More information

General Properties of Radiation Detectors Supplements

General Properties of Radiation Detectors Supplements Phys. 649: Nuclear Techniques Physics Departent Yarouk University Chapter 4: General Properties of Radiation Detectors Suppleents Dr. Nidal M. Ershaidat Overview Phys. 649: Nuclear Techniques Physics Departent

More information

Experimental Design For Model Discrimination And Precise Parameter Estimation In WDS Analysis

Experimental Design For Model Discrimination And Precise Parameter Estimation In WDS Analysis City University of New York (CUNY) CUNY Acadeic Works International Conference on Hydroinforatics 8-1-2014 Experiental Design For Model Discriination And Precise Paraeter Estiation In WDS Analysis Giovanna

More information

An Adaptive UKF Algorithm for the State and Parameter Estimations of a Mobile Robot

An Adaptive UKF Algorithm for the State and Parameter Estimations of a Mobile Robot Vol. 34, No. 1 ACTA AUTOMATICA SINICA January, 2008 An Adaptive UKF Algorith for the State and Paraeter Estiations of a Mobile Robot SONG Qi 1, 2 HAN Jian-Da 1 Abstract For iproving the estiation accuracy

More information

Numerical simulations of isotropic and die compaction of powder by the discrete element method

Numerical simulations of isotropic and die compaction of powder by the discrete element method Nuerical siulations of isotropic and die copaction of powder by the discrete eleent ethod J-F. Jerier, B. Harthong, B. Chareyre, D. Ibault, F-V. Donzé & P. Doréus Laboratoire Sols, Solides, Structures,

More information

OSCILLATIONS AND WAVES

OSCILLATIONS AND WAVES OSCILLATIONS AND WAVES OSCILLATION IS AN EXAMPLE OF PERIODIC MOTION No stories this tie, we are going to get straight to the topic. We say that an event is Periodic in nature when it repeats itself in

More information

Block designs and statistics

Block designs and statistics Bloc designs and statistics Notes for Math 447 May 3, 2011 The ain paraeters of a bloc design are nuber of varieties v, bloc size, nuber of blocs b. A design is built on a set of v eleents. Each eleent

More information

Physics 2210 Fall smartphysics 20 Conservation of Angular Momentum 21 Simple Harmonic Motion 11/23/2015

Physics 2210 Fall smartphysics 20 Conservation of Angular Momentum 21 Simple Harmonic Motion 11/23/2015 Physics 2210 Fall 2015 sartphysics 20 Conservation of Angular Moentu 21 Siple Haronic Motion 11/23/2015 Exa 4: sartphysics units 14-20 Midter Exa 2: Day: Fri Dec. 04, 2015 Tie: regular class tie Section

More information

16.333: Lecture # 7. Approximate Longitudinal Dynamics Models

16.333: Lecture # 7. Approximate Longitudinal Dynamics Models 16.333: Lecture # 7 Approxiate Longitudinal Dynaics Models A couple ore stability derivatives Given ode shapes found identify sipler odels that capture the ain responses Fall 24 16.333 6 1 More Stability

More information

dt dt THE AIR TRACK (II)

dt dt THE AIR TRACK (II) THE AIR TRACK (II) References: [] The Air Track (I) - First Year Physics Laoratory Manual (PHY38Y and PHYY) [] Berkeley Physics Laoratory, nd edition, McGraw-Hill Book Copany [3] E. Hecht: Physics: Calculus,

More information

Proc. of the IEEE/OES Seventh Working Conference on Current Measurement Technology UNCERTAINTIES IN SEASONDE CURRENT VELOCITIES

Proc. of the IEEE/OES Seventh Working Conference on Current Measurement Technology UNCERTAINTIES IN SEASONDE CURRENT VELOCITIES Proc. of the IEEE/OES Seventh Working Conference on Current Measureent Technology UNCERTAINTIES IN SEASONDE CURRENT VELOCITIES Belinda Lipa Codar Ocean Sensors 15 La Sandra Way, Portola Valley, CA 98 blipa@pogo.co

More information

Hydro-Elastic Criterion for Practical Design

Hydro-Elastic Criterion for Practical Design Hydro-Elastic Criterion for Practical Design Hannes Bogaert ), Mirek Kainski ) ) MARIN, Hydro-Structural Services, Wageningen, Netherlands & Delft University of Technology, Ship Structures Laboratory,

More information

A Simplified Analytical Approach for Efficiency Evaluation of the Weaving Machines with Automatic Filling Repair

A Simplified Analytical Approach for Efficiency Evaluation of the Weaving Machines with Automatic Filling Repair Proceedings of the 6th SEAS International Conference on Siulation, Modelling and Optiization, Lisbon, Portugal, Septeber -4, 006 0 A Siplified Analytical Approach for Efficiency Evaluation of the eaving

More information

Momentum. February 15, Table of Contents. Momentum Defined. Momentum Defined. p =mv. SI Unit for Momentum. Momentum is a Vector Quantity.

Momentum. February 15, Table of Contents. Momentum Defined. Momentum Defined. p =mv. SI Unit for Momentum. Momentum is a Vector Quantity. Table of Contents Click on the topic to go to that section Moentu Ipulse-Moentu Equation The Moentu of a Syste of Objects Conservation of Moentu Types of Collisions Collisions in Two Diensions Moentu Return

More information

Applying Experienced Self-Tuning PID Controllers to Position Control of Slider Crank Mechanisms

Applying Experienced Self-Tuning PID Controllers to Position Control of Slider Crank Mechanisms (00/7) 7 80 Applying Experienced Self-Tuning Controllers to osition Control of Slider Crank Mechaniss Chih-Cheng ao cckao@cc.kyit.edu.tw epartent of Electrical Engineering ao Yuan nstitute of Technology

More information

Computer Model For Sieves Vibrations Analysis, Using an Algorithm Based on the False-Position Method

Computer Model For Sieves Vibrations Analysis, Using an Algorithm Based on the False-Position Method Aerican Journal of Applied Sciences 6 (): 48-56, 9 ISSN 546-939 9 Science Publications Coputer Model For Sieves Vibrations Analysis, Using an Algorith Based on the False-Position Method Dinu I. Stoicovici,

More information

Analyzing Simulation Results

Analyzing Simulation Results Analyzing Siulation Results Dr. John Mellor-Cruey Departent of Coputer Science Rice University johnc@cs.rice.edu COMP 528 Lecture 20 31 March 2005 Topics for Today Model verification Model validation Transient

More information

BALLISTIC PENDULUM. EXPERIMENT: Measuring the Projectile Speed Consider a steel ball of mass

BALLISTIC PENDULUM. EXPERIMENT: Measuring the Projectile Speed Consider a steel ball of mass BALLISTIC PENDULUM INTRODUCTION: In this experient you will use the principles of conservation of oentu and energy to deterine the speed of a horizontally projected ball and use this speed to predict the

More information

Time-of-flight Identification of Ions in CESR and ERL

Time-of-flight Identification of Ions in CESR and ERL Tie-of-flight Identification of Ions in CESR and ERL Eric Edwards Departent of Physics, University of Alabaa, Tuscaloosa, AL, 35486 (Dated: August 8, 2008) The accuulation of ion densities in the bea pipe

More information

2 Q 10. Likewise, in case of multiple particles, the corresponding density in 2 must be averaged over all

2 Q 10. Likewise, in case of multiple particles, the corresponding density in 2 must be averaged over all Lecture 6 Introduction to kinetic theory of plasa waves Introduction to kinetic theory So far we have been odeling plasa dynaics using fluid equations. The assuption has been that the pressure can be either

More information

Analysis and Extraction of Temperature Effects on Natural Frequencies of a Footbridge based on Continuous Dynamic Monitoring

Analysis and Extraction of Temperature Effects on Natural Frequencies of a Footbridge based on Continuous Dynamic Monitoring Analysis and Extraction of Teperature Effects on Natural Frequencies of a Footbridge based on Continuous Dynaic Monitoring Wei-Hua Hu, Carlos Moutinho, Filipe Magalhães, Elsa Caetano & Álvaro Cunha Faculty

More information

Uniaxial compressive stress strain model for clay brick masonry

Uniaxial compressive stress strain model for clay brick masonry Uniaxial copressive stress strain odel for clay brick asonry Heant B. Kaushik, Durgesh C. Rai* and Sudhir K. Jain Departent of Civil Engineering, Indian Institute of Technology Kanpur, Kanpur 208 016,

More information

Intelligent Systems: Reasoning and Recognition. Perceptrons and Support Vector Machines

Intelligent Systems: Reasoning and Recognition. Perceptrons and Support Vector Machines Intelligent Systes: Reasoning and Recognition Jaes L. Crowley osig 1 Winter Seester 2018 Lesson 6 27 February 2018 Outline Perceptrons and Support Vector achines Notation...2 Linear odels...3 Lines, Planes

More information

Model Fitting. CURM Background Material, Fall 2014 Dr. Doreen De Leon

Model Fitting. CURM Background Material, Fall 2014 Dr. Doreen De Leon Model Fitting CURM Background Material, Fall 014 Dr. Doreen De Leon 1 Introduction Given a set of data points, we often want to fit a selected odel or type to the data (e.g., we suspect an exponential

More information

CONTROL SYSTEMS, ROBOTICS, AND AUTOMATION Vol. IX Uncertainty Models For Robustness Analysis - A. Garulli, A. Tesi and A. Vicino

CONTROL SYSTEMS, ROBOTICS, AND AUTOMATION Vol. IX Uncertainty Models For Robustness Analysis - A. Garulli, A. Tesi and A. Vicino UNCERTAINTY MODELS FOR ROBUSTNESS ANALYSIS A. Garulli Dipartiento di Ingegneria dell Inforazione, Università di Siena, Italy A. Tesi Dipartiento di Sistei e Inforatica, Università di Firenze, Italy A.

More information

Elastic Force: A Force Balance: Elastic & Gravitational Force: Force Example: Determining Spring Constant. Some Other Forces

Elastic Force: A Force Balance: Elastic & Gravitational Force: Force Example: Determining Spring Constant. Some Other Forces Energy Balance, Units & Proble Solving: Mechanical Energy Balance ABET Course Outcoes: 1. solve and docuent the solution of probles involving eleents or configurations not previously encountered (e) (e.g.

More information

Q ESTIMATION WITHIN A FORMATION PROGRAM q_estimation

Q ESTIMATION WITHIN A FORMATION PROGRAM q_estimation Foration Attributes Progra q_estiation Q ESTIMATION WITHIN A FOMATION POGAM q_estiation Estiating Q between stratal slices Progra q_estiation estiate seisic attenuation (1/Q) on coplex stratal slices using

More information

Numerical Modeling of Self-Compacting Mortar Flow Using Discrete Element Method

Numerical Modeling of Self-Compacting Mortar Flow Using Discrete Element Method Nuerical Modeling of Self-Copacting Flow Using Discrete Eleent Method - Technical Paper - Miansong HUANG *1, Xuehui AN *, Takayuki OBARA *3 and Masahiro OUCHI *4 ABSTRACT A nuerical odeling of Self-Copacting

More information

In the session you will be divided into groups and perform four separate experiments:

In the session you will be divided into groups and perform four separate experiments: Mechanics Lab (Civil Engineers) Nae (please print): Tutor (please print): Lab group: Date of lab: Experients In the session you will be divided into groups and perfor four separate experients: (1) air-track

More information

Department of Physics Preliminary Exam January 3 6, 2006

Department of Physics Preliminary Exam January 3 6, 2006 Departent of Physics Preliinary Exa January 3 6, 2006 Day 1: Classical Mechanics Tuesday, January 3, 2006 9:00 a.. 12:00 p.. Instructions: 1. Write the answer to each question on a separate sheet of paper.

More information

Envelope frequency Response Function Analysis of Mechanical Structures with Uncertain Modal Damping Characteristics

Envelope frequency Response Function Analysis of Mechanical Structures with Uncertain Modal Damping Characteristics Copyright c 2007 Tech Science Press CMES, vol.22, no.2, pp.129-149, 2007 Envelope frequency Response Function Analysis of Mechanical Structures with Uncertain Modal Daping Characteristics D. Moens 1, M.

More information

COULD A VARIABLE MASS OSCILLATOR EXHIBIT THE LATERAL INSTABILITY?

COULD A VARIABLE MASS OSCILLATOR EXHIBIT THE LATERAL INSTABILITY? Kragujevac J. Sci. 3 (8) 3-44. UDC 53.35 3 COULD A VARIABLE MASS OSCILLATOR EXHIBIT THE LATERAL INSTABILITY? Nebojša Danilović, Milan Kovačević and Vukota Babović Institute of Physics, Faculty of Science,

More information

THERMAL ENDURANCE OF UNREINFORCED UNSATURATED POLYESTERS AND VINYL ESTER RESINS = (1) ln = COMPOSITES & POLYCON 2009

THERMAL ENDURANCE OF UNREINFORCED UNSATURATED POLYESTERS AND VINYL ESTER RESINS = (1) ln = COMPOSITES & POLYCON 2009 Aerican Coposites Manufacturers Association January 15-17, 29 Tapa, FL USA Abstract THERMAL ENDURANCE OF UNREINFORCED UNSATURATED POLYESTERS AND VINYL ESTER RESINS by Thore M. Klaveness, Reichhold AS In

More information

Now multiply the left-hand-side by ω and the right-hand side by dδ/dt (recall ω= dδ/dt) to get:

Now multiply the left-hand-side by ω and the right-hand side by dδ/dt (recall ω= dδ/dt) to get: Equal Area Criterion.0 Developent of equal area criterion As in previous notes, all powers are in per-unit. I want to show you the equal area criterion a little differently than the book does it. Let s

More information