λ w w. (3) w 2 2 λ The obtained equation (4) may be presented in the stationary approximation as follows (5) with the boundary conditions: for = 0

Size: px
Start display at page:

Download "λ w w. (3) w 2 2 λ The obtained equation (4) may be presented in the stationary approximation as follows (5) with the boundary conditions: for = 0"

Transcription

1 International Conference on Methods of Aerophysical Research, ICMAR 28 SIMULATION OF POROUS MATERIAL IMPREGNATION A.V. Fedorov, A.A. Zhilin Khristianovich Institute of Theoretical and Applied Mechanics SB RAS 639, Novosibirsk, Russia, Introduction. A wide use of porous materials of new generation in civil engineering and a number of other industry branches leads to a need in investigating the peculiarities of the mechanism of moisture interaction with porous materials. The work [1], in which the eperimental data on the moisture penetration into a porous material are presented and the dependence of the moisture diffusion coefficient on the moisture content in porous material is determined, is devoted to their study. In the present work, the mathematical modeling of the moisture migration process in a porous skeleton of solid material is carried out. The investigation of the pattern of a flow arising at a porous skeleton contact with water surface and the elucidation of the influence of initial parameters of the system the liquid + the solid on the liquid diffusion peculiarities are the main tasks. Physical-mathematical problem statement. Let us consider a vertically posed beam of porous material (the steam-cured aerocrete) whose side walls are moisture-insulated, and the lower face contacts with water surface. The upper plane is free and has a constant humidity. The impregnation process start corresponds to the moment of time when the beam dry face contacts with a humid medium (t = ). After the contact, a humidity wave propagates into the porous material. The problem is to determine the liquid flow pattern in the porous beam at subsequent (t > ) moments of time. To describe the process under study it is natural to invoke the nonstationary diffusion equation in the following form W t W = D( W ). (1) where D(W) is the diffusion coefficient; W is the humidity; t is the time; is the spatial coordinate. We augment equation (1) by the corresponding initial: for t = : =, W = W, < <l, W = and boundary conditions: for = : W = W, for = l: W/ =. (2) Self-similar approimation. Let us go over to new self-similar variables t and λ = t, in which equation (1) takes the form w λ w w t = + D( w). (3) t 2 λ λ λ The problem (2), (3) was solved numerically by the shooting method and involved two stages. The first stage is the testing. Assume that the diffusion coefficient is constant that is D(w) = const = D, then the diffusion equation may be written in self-similar variables (3) as 2 w λ w w t = + D. (4) 2 t 2 λ λ The obtained equation (4) may be presented in the stationary approimation as follows with the boundary conditions: for = λ λ w = w 2D w = w, for λ = + w =. (5) A.V. Fedorov, A.A. Zhilin, 28 1

2 Section V 1-6 D W.5 Fig. 1. Permeability vs. the diffusion coefficient. Fig. 2. Interpolation of eperimental data ( ) by the eponential function (solid line). The solution of equation (5) has the form w = w λ 1 Erf. (6) 2 D We will compare in the following the liquid flows in a porous body, which is characterized by the minimum and maimum values of the diffusion coefficient and with D = D(w). We consider for this purpose the behavior of the obtained solution versus the diffusion coefficient D. We show in Fig. 1 the solutions for three values of the diffusion coefficient D = 1 1-6, and m 2 /s. It is natural that as the diffusion coefficient reduces the permeability coefficient value decreases an, as a consequence, we have the liquid flow pattern presented in Fig. 1 when curve 2 lies above curve 1 corresponding to a lower value of the permeability coefficient. To improve the method of solving the boundary-value problem for the self-similar flow at D = const equation (5) was solved numerically by a shooting method. As the boundary conditions, the value of the function w() = w and the value of the first derivative w'() = w' were specified at the left boundary. The w value equaled.5 in all cases, and the function slope at point λ = was chosen from the criterion w(λ i ) < ε, where λ i is the finite value of the computational region. For the diffusion coefficient D = m 2 /s the w' value amounted to -.47, for D = it amounted to , and for D = it was equal to.473. The obtained solution is also plotted in Fig. 1. It turned out that the numerical solution coincides completely with the solution obtained analytically. The method of lines was applied for the numerical solution of the boundary-value problem for equation (4) with a subsequent solution of the arising system of ordinary differential equations using a method based on the backward differentiation formula. The numerical solution obtained by the method of lines is also shown in Fig. 1 for three values of diffusion coefficients. The numerical solution of the boundary-value problem for equation (4), which was obtained for large times of the process development, coincides completely with the analytical and numerical solution of stationary equation (5), which was obtained above. The second stage is the general case of a variable diffusion coefficient. Let us obtain the solution of the initial- and boundary-value problem for the original equation (3) for a variable value of the diffusion coefficient. Interpolation of eperimental data of [1] is used to determine the dependence of the diffusion coefficient on humidity. As can be seen (see Fig. 2) the eperimental data are fairly described with the aid of an eponential epression in the following form 8 w wp D( w) = a + cep, c where a = 1.5 1, c = 3 1, w =. 36 and c = p

3 International Conference on Methods of Aerophysical Research, ICMAR 28 w.6.5 a) b) λ **.5.55 w = λ * λ i λ Fig. 3. Influence of the initial humidity on permeability, a) for low values of w, b) for high values of w. In the stationary approimation, equation (3) was solved by the shooting method, its solution for w =.5 is shown in Fig. 1 and in Fig. 3a for different w (in a larger scale). The obtained solution represents the humidity profile in self-similar variables. It can be subdivided into three intervals. The first interval is characterized by a humidity increase from to + to w * for λ *. We replace the point at + with the λ i value, the humidity value at which corresponds to a deviation of the humidity profile from the zero value by the quantity ε = 1 1-4, the λ i values are presented for different initial humidity values in the table (Table 1). The point λ * is marked in Figs. 1 and 3а. Thus, the complete width of the humidity profile in self-similar variables amounts to λ i = The second interval is the interval from point λ = λ * to λ = λ ** (point λ ** is shown in Figs. 1 and 3a). This interval is determined by the wave width after Prandtl (l Pr = 5.621). In the interval under consideration, an abrupt increase in humidity is observed, and the inflection point also lies therein, after which the humidity profile changes from the concave one to a conve one. In this region, there is also the maimum gradient, it corresponds to the coordinate λ ma, the humidity value w ma and to its derivative w' ma. For the initial humidity w =.5 these values correspond to 28.6,.25149, and.8925, respectively (see Table 1). The third interval of the humidity profile starts at λ = λ ** 25.8, and terminates at λ =. In the given interval, the humidity profile has a conve shape and smoothly increases from w ** and adheres to the initial humidity value w specified at the left boundary. The solution of the initial- and boundary-value problem (3), (2) was also carried out in the nonstationary approimation, having the purpose of obtaining a self-similar flow by the pseudounsteady method. Figure 4 shows the humidity profiles obtained at the moments of time t = 1, 1.5, 2, 5, 1, and 1. Note that the humidity profile obtained at the time value 1 coincides with the one obtained above in the stationary approimation. At a further increase in t up to 1 and higher the humidity profile remained invariable that is the same as for t = 1 (see Fig. 4). Thus, we have shown that as t there is a passage to the self-similar liquid flow in a porous sample, this flow type proves to be stable. Initial humidity influence. Let us investigate the initial humidity influence on the flow behavior in the sample. Figure 3 shows the humidity distribution along the self-similar variable λ under the initial humidity variation w varying from.5 to.95 with step.5. At small values of w from to.15 the humidity profile in self-similar variables has the shape of a concave monotonously increasing function in the entire interval of λ values from λ = λ i to. The maimum humidity gradient (w' ma ) lies at the left boundary, thus, the second and third regions do not eist in the interval of w under consideration (see Fig. 3а). Consequently, the impregnation wave front is not realized for such parameters. Within increasing initial humidity w from.15 to 5, a shift of the maimum humidity gradient from the left boundary towards the higher λ values is observed (see Table 1), thus, the second region formation occurs. Starting from w = 5, the first region appears. At a subsequent increase in the initial humidity, a shift of the (λ ma ) location of the maimum humidity gradient towards higher λ values is observed (see Table 1). This is related to the beginning of the phase of an intense growth of the diffusion coefficient depending on humidity (see Fig. 2). 3

4 Section V Table 1. w λ i λ ma w' ma w ma l Pr The following peculiarities are observed as w increases from.5 to.95. Firstly, as the initial humidity increases the predecessor region gradually reduces down to the step size along the selfsimilar variable for w =.75, and then vanishes completely (see Figs. 3a and 3b). Secondly, there is a gradual reduction of the wave width after Prandtl, and for w =.7 the formation of an internal discontinuity is observed for λ ma = and the value w ma = At a further increase in the initial humidity up to w =.75 and so on, the discontinuity amplitude increases, and the etension of the second region that is the wave width reduces (l Pr ). Finally, a considerable nearly two-fold increase in the etension of the third region during each step w =.5 is observed. This means that a wave mechanism of the impregnation is organized when an abrupt increase in saturation occurs in a region of small etension. Then the humidity relaation proceeds up to the boundary value in the etended zone. Hence, at large values of the initial humidity, the humidity profile in self-similar variables has an etended smoothly increasing conve form starting from the jump in which the humidity increases from zero to w ** (Fig. 3b). Solution in the region of physical variables. Let us go over to the posed problem solution in the plane of physical variables and t. The solution of the initial- and boundary-value problem (1), (2) was carried out numerically by the above-tested method..5 w t = (1) 1 5 λ Fig. 4. Obtaining of a stationary humidity profile by the pseudo-unsteady method in the self-similar approimation. 4

5 International Conference on Methods of Aerophysical Research, ICMAR 28 W a).2 t = W b) W.6 t = c) t = Fig. 5. Propagation of the humidity wave a) W =, b) W =.5, c) W =.7. Humidity wave propagation. Figure 5 shows the distribution of humidity profiles for moments of time 1 1 with step 1, 1 1 with step 1, and 1 1 with step 1 for three values of the initial humidity: W = (Fig. 5 а), W =.5 (Fig. 5 b), and W =.7 (Fig. 5 c), and Table 2 presents the values of main parameters of the humidity profiles. Analyzing the humidity profiles for W = one can note that as the time increases an intense growth of the filtration impregnation occurs that is i >> ma. With increasing t the humidity profile slope becomes more slanted, and the maimum humidity gradient value becomes less that is W' ma, and as a consequence of this, an increase in the width after Prandtl of the humidity wave width occurs. 5

6 Section V Table 2. W t i ma W' ma W ma L Pr As W increases up to.5 the picture of the humidity profile propagation changes considerably, in particular, the propagation velocity of the filtration predecessor remains nearly the same as for the above-considered case of W =, and the profile inflection point (the wave center) has accelerated and amounted to about 5 % of the predecessor velocity. A nearly two-fold narrowing of the wave width after Prandtl in comparison with the case of W = has also occurred (see Table 2). A further increase in the initial humidity up to.7 leads to a change in the humidity profile form. In particular, the humidity profile has a small filtration region, an abrupt spasmodic growth, and a subsequent etended increase up to the value at the left boundary, which is, however, small in its amplitude. As the moisture propagates into the porous material the humidity profile slope increases, but the humidity wave width after Prandtl is nearly 8 times lower than for W =.5 and by 16 times lower than for W =. Note that the propagation velocity of the humidity wave has increased considerably, by a factor of nearly 1 as compared to the case of W =.5. As is seen in Fig. 5c the main alteration in the humidity profile occurs in the third region. Its etent rapidly increases and begins to take practically the entire width of the humidity profile. Note that as the time increases the propagation velocity of the humidity profile slows down, so in the time interval from 1 to 1 the velocity decreases by 1 times. And a similar trend is observed for W =.5 and. One more peculiarity is the location of the humidity maimum gradient point or the inflection over the profile height at W = W ma.22, which amounts to 73 %; at W =.5 W ma.25, it amounts to 5 %, and for W =.7 W ma.25, it amounts to 35 %. Thus, the inflection point shifts along the profile from the very top (1 %) downwards and stops near the value W ma.26 or about 3 % of the entire profile height for W =.9. 6

7 International Conference on Methods of Aerophysical Research, ICMAR 28.5 W, w t = 1 l = 1 1 1, λ Fig. 6. Comparison of computational results obtained in the plane of physical variables (solid line) and the self-similar approimation (dotted line). For the initial humidity W =.5 the test series of computations was eecuted whose results are presented in Fig. 6. The solid line shows here the humidity profiles obtained at the solution of problem (1), (2) in the physical plane of the motion at the moments of time t = 1, 1, 1 and the computational region etension l = 1, 1, and l = 1, respectively. A feature of the mapping is the alteration of scale of the abscissa ais because at a passage from l = 1 to 1, and then to 1 the ais scale increases by one order of magnitude. The thick dashed line shows the computed results obtained at the solution of the initial- and boundary-value problem (3) and (2) in selfsimilar variables for the moments of time t = 1 and t = 1 (1) (these lines were presented above in Fig. 4 in the form of solid lines). Note that relation l t equals 1 for all three cases. The solution obtained in the plane of physical variables is seen to coincide with the solution obtained in the self-similar approimation. W = 9 mm Fig. 7. Humidity distribution over the section. t, h 7

8 Section V, mm W Table 3. Moisture distribution over the section of porous material. Let us investigate the dynamics of moisture variation in sections 1, 2,, 9 mm in the beam of a porous material whose length l = 1 mm. Figure 7 shows the moisture distribution in the sections under consideration versus time. The humidity profile in each section may be subdivided into three intervals. The first interval (I) is characterized by a zero humidity value, it starts from the time of the eperiment beginning and terminates by the time when the humidity wave reaches the section under consideration. In the second interval (II), the humidity increases smoothly up to W К. The third interval (III) is characterized by a constant humidity value as the first interval, but the constant humidity value equals W К. The finite humidity values in the sections for different values of the initial humidity are presented in Table. 3. Note the features arising at the initial humidity variation. As the section under consideration shifts from the plane of contact with water into the beam depth an increase in interval I is observed. When W =.1 the interval II of the passage from W to W К, is the most etended and amounts to about 1 hours, and it is characterized by the minimum gradient. The W К value varies considerably depending on the section, so at a passage from section 1 to 9 mm the variation of W К makes 8 %. As W increases from.1 to.4 an insignificant reduction of the transition region II occurs, and the variation of the W К values remains practically within the same ranges. At W =.5 the transition region II is narrowing and amounts to about 1 hours, and the range of the W К variation amounts to about 25 %. An increase in W from.5 to.9 is characterized by an intense narrowing of interval II from hours to minutes and seconds. The slope gradient increases considerably and reaches a discontinuous one, and the range of the W К values is narrowing. At W =.9 the humidity transition (II) from W to W К becomes very narrow and spasmodic and amounts to about 5 seconds, and the deviation of W К varies by no more than.5 % depending on the section. Mathematical model verification. A comparison of the results of numerical computations eecuted by the proposed mathematical model with eperimental data obtained in the work [1] has been carried out. As is seen in Fig. 7, the proposed mathematical model adequately describes the eperimental data (cross sections = 4 and 6 mm). Conclusions. 1. A diffusion physical and mathematical model of the capillary impregnation of a porous material, which is based on the obtained analytical epression for the diffusion coefficient describing fairly the eperimental data, has been proposed and verified. 2. The mathematical technology for solving the one-dimensional nonstationary problems of impregnation has been developed and tested on a self-similar solution of the corresponding boundary-value impregnation problem. 3. It has turned out that at large times of the impregnation process development, the liquid flow in the sample is described by a solution of the self-similar type. Its stability is shown. 8

9 International Conference on Methods of Aerophysical Research, ICMAR Depending on the initial humidity at the sample boundary it proved to be possible to give a classification of the moisture diffusion in the form of: a smooth impregnation wave, a diffusion impregnation wave followed by a predecessor ahead of the transitional structure and a diffusion relaation zone towards the boundary value of saturation, a wave with an abrupt change of the profile in the wave head. The work was made under a partial financial support of the Russian Foundation for Basic Research (grant No ), the grant of the Russian Federation President MK REFERENCES 1. Nisovtsev M.I., Stankus S.V., Sterlyagov A.N., Terekhov V.I. and Khairulin R.A. Eperimental determination of moisture diffusion coefficients in porous materials at a capillary and sorption moistening // J. Eng. Phys. 25. Vol. 78, No. 1. P

EXCITATION OF GÖRTLER-INSTABILITY MODES IN CONCAVE-WALL BOUNDARY LAYER BY LONGITUDINAL FREESTREAM VORTICES

EXCITATION OF GÖRTLER-INSTABILITY MODES IN CONCAVE-WALL BOUNDARY LAYER BY LONGITUDINAL FREESTREAM VORTICES ICMAR 2014 EXCITATION OF GÖRTLER-INSTABILITY MODES IN CONCAVE-WALL BOUNDARY LAYER BY LONGITUDINAL FREESTREAM VORTICES Introduction A.V. Ivanov, Y.S. Kachanov, D.A. Mischenko Khristianovich Institute of

More information

n v molecules will pass per unit time through the area from left to

n v molecules will pass per unit time through the area from left to 3 iscosity and Heat Conduction in Gas Dynamics Equations of One-Dimensional Gas Flow The dissipative processes - viscosity (internal friction) and heat conduction - are connected with existence of molecular

More information

THE EFFECT OF POROUS BLOWING AND SUCTION ON AERODYNAMICS AND HEAT TRANSFER IN SEPARATED LAMINAR FLOW IN DUCT BEHIND OF BACKWARD-FACING STEP S.R.

THE EFFECT OF POROUS BLOWING AND SUCTION ON AERODYNAMICS AND HEAT TRANSFER IN SEPARATED LAMINAR FLOW IN DUCT BEHIND OF BACKWARD-FACING STEP S.R. THE EFFECT OF POROUS BLOWING AND SUCTION ON AERODYNAMICS AND HEAT TRANSFER IN SEPARATED LAMINAR FLOW IN DUCT BEHIND OF BACKWARD-FACING STEP S.R. Batenko,A.P.Grechanova, and V.I. Terekhov S.S. Kutateladze

More information

MORE CURVE SKETCHING

MORE CURVE SKETCHING Mathematics Revision Guides More Curve Sketching Page of 3 MK HOME TUITION Mathematics Revision Guides Level: AS / A Level MEI OCR MEI: C4 MORE CURVE SKETCHING Version : 5 Date: 05--007 Mathematics Revision

More information

HEAT AND MASS TRANSFER IN A HIGH-POROUS LOW- TEMPERATURE THERMAL INSULATION IN REAL OPERATING CONDITIONS

HEAT AND MASS TRANSFER IN A HIGH-POROUS LOW- TEMPERATURE THERMAL INSULATION IN REAL OPERATING CONDITIONS MATEC Web of Conferences 3, 0033 ( 05) DOI: 0.05/ matecconf/ 0530033 C Owned by the authors, published by EDP Sciences, 05 HEAT AND MASS TRANSFER IN A HIGH-POROUS LOW- TEMPERATURE THERMAL INSULATION IN

More information

Properties of Derivatives

Properties of Derivatives 6 CHAPTER Properties of Derivatives To investigate derivatives using first principles, we will look at the slope of f ( ) = at the point P (,9 ). Let Q1, Q, Q, Q4, be a sequence of points on the curve

More information

Fig. 1. The coordinate system and the directions of the velocities.

Fig. 1. The coordinate system and the directions of the velocities. ICMAR 201 FLOW STABILITY NEAR A PLATE WITH A SURFACE MOVING AGAINST AN INCOMING STREAM A.M. Gaifullin, N.N. Kiselev, A.A. Kornyakov The Central Aerohydrodynamic Institute 10180, Zhukovsky, Moscow Reg.,

More information

NUMERICAL SIMULATION OF LONG WAVE RUNUP ON A SLOPING BEACH*

NUMERICAL SIMULATION OF LONG WAVE RUNUP ON A SLOPING BEACH* NUMERICAL SIMULATION OF LONG WAVE RUNUP ON A SLOPING BEACH* * presented at Long Waves Symposium (in parallel with the XXX IAHR Congress) August 5-7, 003, AUTh, Thessaloniki, Greece. by HAKAN I. TARMAN

More information

A First Jump of Microgel; Actuation Speed Enhancement by Elastic Instability

A First Jump of Microgel; Actuation Speed Enhancement by Elastic Instability Electronic Supplementary Information (ESI) for A First Jump of Microgel; Actuation Speed Enhancement by Elastic Instability Howon Lee, Chunguang Xia and Nicholas X. Fang* Department of Mechanical Science

More information

Phase shift s influence of two strong pulsed laser waves on effective interaction of electrons

Phase shift s influence of two strong pulsed laser waves on effective interaction of electrons Phase shift s influence of two strong pulsed laser waves on effective interaction of electrons S S Starodub, S P Roshchupkin and V V Dubov Institute of Applied Physics, National Academy of Sciences of

More information

Numerical simulation of the sound waves interaction with a supersonic boundary layer

Numerical simulation of the sound waves interaction with a supersonic boundary layer Numerical simulation of the sound waves interaction with a supersonic boundary layer S. A. GAPONOV A.N. SEMENOV Khristianovich Institute of Theoretical and Applied Mechanics Novosibirsk 0090 RUSSIA gaponov@itam.nsc.ru

More information

Maximum and Minimum Values

Maximum and Minimum Values Maimum and Minimum Values y Maimum Minimum MATH 80 Lecture 4 of 6 Definitions: A function f has an absolute maimum at c if f ( c) f ( ) for all in D, where D is the domain of f. The number f (c) is called

More information

CALCULATION OF PRESSURE FIELD IN THE PROBLEM OF SONIC BOOM FROM VARIOUS THIN AXISYMMETRIC BODIES

CALCULATION OF PRESSURE FIELD IN THE PROBLEM OF SONIC BOOM FROM VARIOUS THIN AXISYMMETRIC BODIES CALCULATION OF PRESSURE FIELD IN THE PROBLEM OF SONIC BOOM FROM VARIOUS THIN AXISYMMETRIC BODIES А.V. Potapkin, D.Yu. Moskvichev Khristianovich Institute of Theoretical and Applied Mechanics SB RAS 630090,

More information

Poiseuille Advection of Chemical Reaction Fronts

Poiseuille Advection of Chemical Reaction Fronts Utah State University DigitalCommons@USU All Physics Faculty Publications Physics 8- Poiseuille Advection of Chemical Reaction Fronts Boyd F. Edwards Utah State University Follow this and additional works

More information

Solution of Partial Differential Equations

Solution of Partial Differential Equations Solution of Partial Differential Equations Introduction and Problem Statement Combination of Variables R. Shankar Subramanian We encounter partial differential equations routinely in transport phenomena.

More information

Exponential Growth and Decay - M&M's Activity

Exponential Growth and Decay - M&M's Activity Eponential Growth and Decay - M&M's Activity Activity 1 - Growth 1. The results from the eperiment are as follows: Group 1 0 4 1 5 2 6 3 4 15 5 22 6 31 2. The scatterplot of the result is as follows: 3.

More information

International Conference on Methods of Aerophysical Research, ICMAR secondary gas ( p0s. aerodynamic throat. subsonic diffuser.

International Conference on Methods of Aerophysical Research, ICMAR secondary gas ( p0s. aerodynamic throat. subsonic diffuser. OPTIMIZATION OF GAS-JET EJECTORS WITH CONVERGING CHAMBER A.V. Sobolev Khristianovich Institute of Theoretical and Applied Mechanics, SD RAS, Novosibirs 630090, Russia In the development of gas-jet ejectors,

More information

ON A MECHANISM OF INTRAPHASE INTERACTION IN NON-RELAXING TWO-PHASE FLOW V.M.

ON A MECHANISM OF INTRAPHASE INTERACTION IN NON-RELAXING TWO-PHASE FLOW V.M. ON A MECHANISM OF INTRAPHASE INTERACTION IN NON-RELAXING TWO-PHASE FLOW V.M. Boiko, K.V. Klinkov, and S.V. Poplavski Institute of Theoretical and Applied Mechanics SB RAS, 630090 Novosibirsk, Russia 1.

More information

Pre-Calculus Module 4

Pre-Calculus Module 4 Pre-Calculus Module 4 4 th Nine Weeks Table of Contents Precalculus Module 4 Unit 9 Rational Functions Rational Functions with Removable Discontinuities (1 5) End Behavior of Rational Functions (6) Rational

More information

NATURAL CONVECTION IN INCLINED RECTANGULAR POROUS CAVITY SUBJECT TO HEAT FLUXES ON THE LONG SIDE WALLS

NATURAL CONVECTION IN INCLINED RECTANGULAR POROUS CAVITY SUBJECT TO HEAT FLUXES ON THE LONG SIDE WALLS Proceedings of 4 th ICCHMT May 7 0, 005, Paris-Cachan, FRANCE ICCHMT 05-53 NATURAL CONVECTION IN INCLINED RECTANGULAR POROUS CAVITY SUBJECT TO HEAT FLUXES ON THE LONG SIDE WALLS L. Storesletten*, D.A.S.

More information

Salt Crystallization in Hydrophobic Porous Materials

Salt Crystallization in Hydrophobic Porous Materials Hydrophobe V 5 th International Conference on Water Repellent Treatment of Building Materials Aedificatio Publishers, 97-16 (28) Salt Crystallization in Hydrophobic Porous Materials H. Derluyn 1, A.S.

More information

Artificial Neuron (Perceptron)

Artificial Neuron (Perceptron) 9/6/208 Gradient Descent (GD) Hantao Zhang Deep Learning with Python Reading: https://en.wikipedia.org/wiki/gradient_descent Artificial Neuron (Perceptron) = w T = w 0 0 + + w 2 2 + + w d d where

More information

CHAPTER 11: CHROMATOGRAPHY FROM A MOLECULAR VIEWPOINT

CHAPTER 11: CHROMATOGRAPHY FROM A MOLECULAR VIEWPOINT CHAPTER 11: CHROMATOGRAPHY FROM A MOLECULAR VIEWPOINT Contrasting approaches 1. bulk transport (e.g., c c = W ) t x + D c x goal: track concentration changes advantage: mathematical rigor (for simple models).

More information

Advanced Hydrology Prof. Dr. Ashu Jain Department of Civil Engineering Indian Institute of Technology, Kanpur. Lecture 6

Advanced Hydrology Prof. Dr. Ashu Jain Department of Civil Engineering Indian Institute of Technology, Kanpur. Lecture 6 Advanced Hydrology Prof. Dr. Ashu Jain Department of Civil Engineering Indian Institute of Technology, Kanpur Lecture 6 Good morning and welcome to the next lecture of this video course on Advanced Hydrology.

More information

International Conference on Methods of Aerophysical Research, ICMAR 2008

International Conference on Methods of Aerophysical Research, ICMAR 2008 International Conference on Methods of Aerophysical Research, ICMAR 8 EXPERIMENTAL STUDY OF UNSTEADY EFFECTS IN SHOCK WAVE / TURBULENT BOUNDARY LAYER INTERACTION P.A. Polivanov, А.А. Sidorenko, A.A. Maslov

More information

1. Find A and B so that f x Axe Bx. has a local minimum of 6 when. x 2.

1. Find A and B so that f x Axe Bx. has a local minimum of 6 when. x 2. . Find A and B so that f Ae B has a local minimum of 6 when.. The graph below is the graph of f, the derivative of f; The domain of the derivative is 5 6. Note there is a cusp when =, a horizontal tangent

More information

Solutions to Homework 8, Mathematics 1

Solutions to Homework 8, Mathematics 1 Solutions to Homework 8, Mathematics Problem [6 points]: Do the detailed graphing definition domain, intersections with the aes, its at ±, monotonicity, local and global etrema, conveity/concavity, inflection

More information

Chapter 4 (Lecture 6-7) Schrodinger equation for some simple systems Table: List of various one dimensional potentials System Physical correspondence

Chapter 4 (Lecture 6-7) Schrodinger equation for some simple systems Table: List of various one dimensional potentials System Physical correspondence V, E, Chapter (Lecture 6-7) Schrodinger equation for some simple systems Table: List of various one dimensional potentials System Physical correspondence Potential Total Energies and Probability density

More information

an inverse problem of thickness design for single layer textile material under low temperature. Dinghua Xu, Jianxin Cheng, Xiaohong Zhou

an inverse problem of thickness design for single layer textile material under low temperature. Dinghua Xu, Jianxin Cheng, Xiaohong Zhou Journal of Math-for-Industry, Vol.(B-4), pp.39 46 An inverse problem of thickness design for single layer tetile material under low temperature Dinghua Xu, Jianin Cheng, Xiaohong Zhou Received on August,

More information

7.4 The Elementary Beam Theory

7.4 The Elementary Beam Theory 7.4 The Elementary Beam Theory In this section, problems involving long and slender beams are addressed. s with pressure vessels, the geometry of the beam, and the specific type of loading which will be

More information

Key ideas about dynamic models

Key ideas about dynamic models GSTDMB 202: DYNAMICAL MODELLING FOR BIOLOGY AND MEDICINE Lecture 2 Introduction to modelling with differential equations Markus Owen ey ideas about dynamic models Dynamic models describe the change in

More information

Section 3.3 Limits Involving Infinity - Asymptotes

Section 3.3 Limits Involving Infinity - Asymptotes 76 Section. Limits Involving Infinity - Asymptotes We begin our discussion with analyzing its as increases or decreases without bound. We will then eplore functions that have its at infinity. Let s consider

More information

Structure of Periodic Cavitation Clouds in Submerged Impinging Water-Jet Issued from Horn-Type Nozzle

Structure of Periodic Cavitation Clouds in Submerged Impinging Water-Jet Issued from Horn-Type Nozzle 9th Pacific Rim International Conference on Water Jetting Technology Structure of Periodic Cavitation Clouds in Submerged Impinging Water-Jet Issued from Horn-Type Nole Keiichi SATO a*, Yasuhiro SUGIMOTO

More information

Continuum Modelling of Traffic Flow

Continuum Modelling of Traffic Flow Continuum Modelling of Traffic Flow Christopher Lustri June 16, 2010 1 Introduction We wish to consider the problem of modelling flow of vehicles within a traffic network. In the past, stochastic traffic

More information

Chapter 10. Solids and Fluids

Chapter 10. Solids and Fluids Chapter 10 Solids and Fluids Surface Tension Net force on molecule A is zero Pulled equally in all directions Net force on B is not zero No molecules above to act on it Pulled toward the center of the

More information

About Some Features of a Magma Flow Structure at Explosive Volcano Eruptions

About Some Features of a Magma Flow Structure at Explosive Volcano Eruptions About Some Features of a Magma Flow Structure at Explosive Volcano Eruptions V. Kedrinskiy 1 Introduction The cyclic character of magma ejections is one of the basic aspects in the research field of the

More information

4.3 How derivatives affect the shape of a graph. The first derivative test and the second derivative test.

4.3 How derivatives affect the shape of a graph. The first derivative test and the second derivative test. Chapter 4: Applications of Differentiation In this chapter we will cover: 41 Maimum and minimum values The critical points method for finding etrema 43 How derivatives affect the shape of a graph The first

More information

A Padé approximation to the scalar wavefield extrapolator for inhomogeneous media

A Padé approximation to the scalar wavefield extrapolator for inhomogeneous media A Padé approimation A Padé approimation to the scalar wavefield etrapolator for inhomogeneous media Yanpeng Mi, Zhengsheng Yao, and Gary F. Margrave ABSTRACT A seismic wavefield at depth z can be obtained

More information

Commun Nonlinear Sci Numer Simulat

Commun Nonlinear Sci Numer Simulat Commun Nonlinear Sci Numer Simulat 7 (0) 3499 3507 Contents lists available at SciVerse ScienceDirect Commun Nonlinear Sci Numer Simulat journal homepage: www.elsevier.com/locate/cnsns Application of the

More information

Answers. Investigation 2. ACE Assignment Choices. Applications. Problem 2.5. Problem 2.1. Problem 2.2. Problem 2.3. Problem 2.4

Answers. Investigation 2. ACE Assignment Choices. Applications. Problem 2.5. Problem 2.1. Problem 2.2. Problem 2.3. Problem 2.4 Answers Investigation ACE Assignment Choices Problem. Core, Problem. Core, Other Applications ; Connections, 3; unassigned choices from previous problems Problem.3 Core Other Connections, ; unassigned

More information

Current-Voltage Characteristics for p-i-p Diodes. Angel Mancebo Under the guidance of Selman Hershfield

Current-Voltage Characteristics for p-i-p Diodes. Angel Mancebo Under the guidance of Selman Hershfield Current-oltage Characteristics for p-i-p Diodes Angel Mancebo Under the guidance of Selman Hershfield Department of Physics, University of Florida, Gainesville, FL 326 Abstract We solve numerically the

More information

BE SURE TO READ THE DIRECTIONS PAGE & MAKE YOUR NOTECARDS FIRST!! Part I: Unlimited and Continuous! (21 points)

BE SURE TO READ THE DIRECTIONS PAGE & MAKE YOUR NOTECARDS FIRST!! Part I: Unlimited and Continuous! (21 points) BE SURE TO READ THE DIRECTIONS PAGE & MAKE YOUR NOTECARDS FIRST!! Part I: United and Continuous! ( points) For #- below, find the its, if they eist.(#- are pt each) ) 7 ) 9 9 ) 5 ) 8 For #5-7, eplain why

More information

AP Calculus (BC) Summer Assignment (169 points)

AP Calculus (BC) Summer Assignment (169 points) AP Calculus (BC) Summer Assignment (69 points) This packet is a review of some Precalculus topics and some Calculus topics. It is to be done NEATLY and on a SEPARATE sheet of paper. Use your discretion

More information

November 13, 2018 MAT186 Week 8 Justin Ko

November 13, 2018 MAT186 Week 8 Justin Ko 1 Mean Value Theorem Theorem 1 (Mean Value Theorem). Let f be a continuous on [a, b] and differentiable on (a, b). There eists a c (a, b) such that f f(b) f(a) (c) =. b a Eample 1: The Mean Value Theorem

More information

ax, From AtoB bx c, From BtoC

ax, From AtoB bx c, From BtoC Name: Date: Block: Semester Assessment Revision 3 Multiple Choice Calculator Active NOTE: The eact numerical value of the correct answer may not always appear among the choices given. When this happens,

More information

MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. B) 94 C) ) A) 1 2

MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. B) 94 C) ) A) 1 2 Chapter Calculus MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. Find the average rate of change of the function over the given interval. ) = 73-5

More information

Chapter (AB/BC, non-calculator) (a) Find the critical numbers of g. (b) For what values of x is g increasing? Justify your answer.

Chapter (AB/BC, non-calculator) (a) Find the critical numbers of g. (b) For what values of x is g increasing? Justify your answer. Chapter 3 1. (AB/BC, non-calculator) Given g ( ) 2 4 3 6 : (a) Find the critical numbers of g. (b) For what values of is g increasing? Justify your answer. (c) Identify the -coordinate of the critical

More information

Chapter 6. Nonlinear Equations. 6.1 The Problem of Nonlinear Root-finding. 6.2 Rate of Convergence

Chapter 6. Nonlinear Equations. 6.1 The Problem of Nonlinear Root-finding. 6.2 Rate of Convergence Chapter 6 Nonlinear Equations 6. The Problem of Nonlinear Root-finding In this module we consider the problem of using numerical techniques to find the roots of nonlinear equations, f () =. Initially we

More information

SERVICEABILITY OF BEAMS AND ONE-WAY SLABS

SERVICEABILITY OF BEAMS AND ONE-WAY SLABS CHAPTER REINFORCED CONCRETE Reinforced Concrete Design A Fundamental Approach - Fifth Edition Fifth Edition SERVICEABILITY OF BEAMS AND ONE-WAY SLABS A. J. Clark School of Engineering Department of Civil

More information

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin.

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin. THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY 1. Introduction V. A. Sharifulin Perm State Technical Universit, Perm, Russia e-mail: sharifulin@perm.ru Water

More information

Reference Trajectory Generation for an Atomic Force Microscope

Reference Trajectory Generation for an Atomic Force Microscope Mechatronics 2010, June 28-30, Swiss Federal Institute of Technology ETH, Zurich Switzerland 1 Reference Trajectory Generation for an Atomic Force Microscope Ivan Furlan and Silvano Balemi 1 Department

More information

Approximate inference, Sampling & Variational inference Fall Cours 9 November 25

Approximate inference, Sampling & Variational inference Fall Cours 9 November 25 Approimate inference, Sampling & Variational inference Fall 2015 Cours 9 November 25 Enseignant: Guillaume Obozinski Scribe: Basile Clément, Nathan de Lara 9.1 Approimate inference with MCMC 9.1.1 Gibbs

More information

Chiang/Wainwright: Fundamental Methods of Mathematical Economics

Chiang/Wainwright: Fundamental Methods of Mathematical Economics Chiang/Wainwright: Fundamental Methods of Mathematical Economics CHAPTER 9 EXERCISE 9.. Find the stationary values of the following (check whether they are relative maima or minima or inflection points),

More information

18.01 Single Variable Calculus Fall 2006

18.01 Single Variable Calculus Fall 2006 MIT OpenCourseWare http://ocw.mit.edu 8.0 Single Variable Calculus Fall 2006 For information about citing these materials or our Terms of Use, visit: http://ocw.mit.edu/terms. Lecture 0 8.0 Fall 2006 Lecture

More information

Calculus 1st Semester Final Review

Calculus 1st Semester Final Review Calculus st Semester Final Review Use the graph to find lim f ( ) (if it eists) 0 9 Determine the value of c so that f() is continuous on the entire real line if f ( ), c /, > 0 Find the limit: lim 6+

More information

CHAPTER 2: Partial Derivatives. 2.2 Increments and Differential

CHAPTER 2: Partial Derivatives. 2.2 Increments and Differential CHAPTER : Partial Derivatives.1 Definition of a Partial Derivative. Increments and Differential.3 Chain Rules.4 Local Etrema.5 Absolute Etrema 1 Chapter : Partial Derivatives.1 Definition of a Partial

More information

Math Honors Calculus I Final Examination, Fall Semester, 2013

Math Honors Calculus I Final Examination, Fall Semester, 2013 Math 2 - Honors Calculus I Final Eamination, Fall Semester, 2 Time Allowed: 2.5 Hours Total Marks:. (2 Marks) Find the following: ( (a) 2 ) sin 2. (b) + (ln 2)/(+ln ). (c) The 2-th Taylor polynomial centered

More information

AP Calculus (BC) Summer Assignment (104 points)

AP Calculus (BC) Summer Assignment (104 points) AP Calculus (BC) Summer Assignment (0 points) This packet is a review of some Precalculus topics and some Calculus topics. It is to be done NEATLY and on a SEPARATE sheet of paper. Use your discretion

More information

Steady One-Dimensional Diffusion of One Species A through a Second Non-Transferring Species B. z y x. Liquid A

Steady One-Dimensional Diffusion of One Species A through a Second Non-Transferring Species B. z y x. Liquid A Steady One-Dimensional Diffusion of One Species through a Second on-transferring Species B R. Shankar Subramanian Department of Chemical and Biomolecular Engineering Clarkson University Consider a simple

More information

Earthquake Loads According to IBC IBC Safety Concept

Earthquake Loads According to IBC IBC Safety Concept Earthquake Loads According to IBC 2003 The process of determining earthquake loads according to IBC 2003 Spectral Design Method can be broken down into the following basic steps: Determination of the maimum

More information

arxiv:hep-ph/ v1 18 Dec 2002

arxiv:hep-ph/ v1 18 Dec 2002 Interference of Conversion and Bremsstrahlung Amplitudes in the Decay K L µ + µ γ arxiv:hep-ph/22262v 8 Dec 22 P. Poulose and L. M. Sehgal Institute of Theoretical Physics E, RWTH Aachen, D-5256 Aachen,

More information

A Computer Controlled Microwave Spectrometer for Dielectric Relaxation Studies of Polar Molecules

A Computer Controlled Microwave Spectrometer for Dielectric Relaxation Studies of Polar Molecules 384 A Computer Controlled Microave Spectrometer for Dielectric Relaation Studies of Polar Molecules Jai N. Dahiya*, Santaneel Ghosh and J. A. Roberts+ Department of Physics and Engineering Physics, Southeast

More information

Final Exam Review / AP Calculus AB

Final Exam Review / AP Calculus AB Chapter : Final Eam Review / AP Calculus AB Use the graph to find each limit. 1) lim f(), lim f(), and lim π - π + π f 5 4 1 y - - -1 - - -4-5 ) lim f(), - lim f(), and + lim f 8 6 4 y -4 - - -1-1 4 5-4

More information

KINETIC MODELING OF OXIDATION METHANE CONVERSION IN REGIME OF FILTRATION COMBUSTION WITH SUPERADIABATIC HEATING

KINETIC MODELING OF OXIDATION METHANE CONVERSION IN REGIME OF FILTRATION COMBUSTION WITH SUPERADIABATIC HEATING KINETIC MODELING OF OXIDATION METHANE CONVERSION IN REGIME OF FILTRATION COMBUSTION WITH SUPERADIABATIC HEATING Anna A. Karnaukh, Avigeya N. Ivanova, Svetlana S. Kostenko, George B. Manelis, and Eugene

More information

PECULIARITIES OF RAMJET COMBUSTION CHAMBER WORK WITH RESONATOR UNDER CONDITION OF VIBRATION FUEL COMBUSTION A.V.

PECULIARITIES OF RAMJET COMBUSTION CHAMBER WORK WITH RESONATOR UNDER CONDITION OF VIBRATION FUEL COMBUSTION A.V. PECULIARITIES OF RAMJET COMBUSTION CHAMBER WORK WITH RESONATOR UNDER CONDITION OF VIBRATION FUEL COMBUSTION A.V. Potapkin, A.A. Pavlov, and D.Yu. Moskvichev Institute of Theoretical and Applied mechanics

More information

2008 CALCULUS AB SECTION I, Part A Time 55 minutes Number of Questions 28 A CALCULATOR MAY NOT BE USED ON THIS PART OF THE EXAMINATION

2008 CALCULUS AB SECTION I, Part A Time 55 minutes Number of Questions 28 A CALCULATOR MAY NOT BE USED ON THIS PART OF THE EXAMINATION 8 CALCULUS AB SECTION I, Part A Time 55 minutes Number of Questions 8 A CALCULATOR MAY NOT BE USED ON THIS PART OF THE EXAMINATION Directions: Solve each of the following problems. After eamining the form

More information

SOLUTIONS FOR THEORETICAL COMPETITION Theoretical Question 1 (10 points) 1A (3.5 points)

SOLUTIONS FOR THEORETICAL COMPETITION Theoretical Question 1 (10 points) 1A (3.5 points) II International Zhautkov Olmpiad/Theoretical Competition/Solutions Page 1/10 SOLUTIONS FOR THEORETICAL COMPETITION Theoretical Question 1 (10 points) 1A (.5 points) m v Mu m = + w + ( u w ) + mgr It is

More information

Review of elements of Calculus (functions in one variable)

Review of elements of Calculus (functions in one variable) Review of elements of Calculus (functions in one variable) Mainly adapted from the lectures of prof Greg Kelly Hanford High School, Richland Washington http://online.math.uh.edu/houstonact/ https://sites.google.com/site/gkellymath/home/calculuspowerpoints

More information

DESIGN OF A MULTIMODE AXISYMMETRIC NOZZLE FOR A HYPERSONIC WIND TUNNEL BY METHODS OF NUMERICAL OPTIMIZATION

DESIGN OF A MULTIMODE AXISYMMETRIC NOZZLE FOR A HYPERSONIC WIND TUNNEL BY METHODS OF NUMERICAL OPTIMIZATION International Conference on Methods of Aerophysical Research, ICMAR 2008 DESIGN OF A MULTIMODE AXISYMMETRIC NOZZLE FOR A HYPERSONIC WIND TUNNEL BY METHODS OF NUMERICAL OPTIMIZATION S.M. Aulcheno 1, V.M.

More information

University of Bergen. Solutions to Exam in MAT111 - Calculus 1

University of Bergen. Solutions to Exam in MAT111 - Calculus 1 Universit of Bergen The Facult of Mathematics and Natural Sciences English Solutions to Eam in MAT - Calculus Wednesda Ma 0, 07, 09.00-4.00 Eercise. a) Find the real numbers and such that the comple variable

More information

Numerical modeling of a cutting torch

Numerical modeling of a cutting torch Journal of Physics: Conference Series OPEN ACCESS Numerical modeling of a cutting torch To cite this article: B R Mancinelli et al 2014 J. Phys.: Conf. Ser. 511 012071 View the article online for updates

More information

Chapter 2: The Random Variable

Chapter 2: The Random Variable Chapter : The Random Variable The outcome of a random eperiment need not be a number, for eample tossing a coin or selecting a color ball from a bo. However we are usually interested not in the outcome

More information

THE EXPERIMENTAL STUDY OF THE EFFECT OF ADDING HIGH-MOLECULAR POLYMERS ON HEAT TRANSFER CHARACTERISTICS OF NANOFLUIDS

THE EXPERIMENTAL STUDY OF THE EFFECT OF ADDING HIGH-MOLECULAR POLYMERS ON HEAT TRANSFER CHARACTERISTICS OF NANOFLUIDS THE EXPERIMENTAL STUDY OF THE EFFECT OF ADDING HIGH-MOLECULAR POLYMERS ON HEAT TRANSFER CHARACTERISTICS OF NANOFLUIDS Dmitriy Guzei 1, *, Maxim Pryazhnikov 1, Andrey Minakov 1,, and Vladimir Zhigarev 1

More information

A high order adaptive finite element method for solving nonlinear hyperbolic conservation laws

A high order adaptive finite element method for solving nonlinear hyperbolic conservation laws A high order adaptive finite element method for solving nonlinear hyperbolic conservation laws Zhengfu Xu, Jinchao Xu and Chi-Wang Shu 0th April 010 Abstract In this note, we apply the h-adaptive streamline

More information

MATH section 3.4 Curve Sketching Page 1 of 29

MATH section 3.4 Curve Sketching Page 1 of 29 MATH section. Curve Sketching Page of 9 The step by step procedure below is for regular rational and polynomial functions. If a function contains radical or trigonometric term, then proceed carefully because

More information

Slender Structures Load carrying principles

Slender Structures Load carrying principles Slender Structures Load carrying principles Continuously Elastic Supported (basic) Cases: Etension, shear Euler-Bernoulli beam (Winkler 1867) v2017-2 Hans Welleman 1 Content (preliminary schedule) Basic

More information

AP Calculus BC Summer Assignment 2018

AP Calculus BC Summer Assignment 2018 AP Calculus BC Summer Assignment 018 Name: When you come back to school, I will epect you to have attempted every problem. These skills are all different tools that we will pull out of our toolbo at different

More information

School Year

School Year AP Calculus AB Assignment 06 07 School Year In order to ensure that our AP Calculus classes meet the standards required by the College Board, it is strongly recommended that all calculus students complete

More information

Modeling of liquid and gas flows in the horizontal layer with evaporation

Modeling of liquid and gas flows in the horizontal layer with evaporation Modeling of liquid and gas flows in the horizontal layer with evaporation Yuri Lyulin 1, Ekaterina Rezanova 1,2,* 1 Kutateladze Institute of Thermophysics SB RAS, 1, Lavrentyieva ave., 630090, Novosibirsk,

More information

The Schrödinger Equation in One Dimension

The Schrödinger Equation in One Dimension The Schrödinger Equation in One Dimension Introduction We have defined a comple wave function Ψ(, t) for a particle and interpreted it such that Ψ ( r, t d gives the probability that the particle is at

More information

Chapter 5. Static Non-Linear Analysis of Parallel Kinematic XY Flexure Mechanisms

Chapter 5. Static Non-Linear Analysis of Parallel Kinematic XY Flexure Mechanisms Chapter 5. Static Non-Linear Analysis of Parallel Kinematic XY Fleure Mechanisms In this chapter we present the static non-linear analysis for some of the XY fleure mechanism designs that were proposed

More information

1.105 Solid Mechanics Laboratory Fall 2003

1.105 Solid Mechanics Laboratory Fall 2003 1.105 Solid Mechanics Laboratory Fall 2003 Eperiment 6 The linear, elastic behavior of a Beam The objectives of this eperiment are To eperimentally study the linear elastic behavior of beams under four

More information

PART A: Answer in the space provided. Each correct answer is worth one mark each.

PART A: Answer in the space provided. Each correct answer is worth one mark each. PART A: Answer in the space provided. Each correct answer is worth one mark each. 1. Find the slope of the tangent to the curve at the point (,6). =. If the tangent line to the curve k( ) = is horizontal,

More information

Lecture 12: Transcritical flow over an obstacle

Lecture 12: Transcritical flow over an obstacle Lecture 12: Transcritical flow over an obstacle Lecturer: Roger Grimshaw. Write-up: Erinna Chen June 22, 2009 1 Introduction The flow of a fluid over an obstacle is a classical and fundamental problem

More information

The stationary points will be the solutions of quadratic equation x

The stationary points will be the solutions of quadratic equation x Calculus 1 171 Review In Problems (1) (4) consider the function f ( ) ( ) e. 1. Find the critical (stationary) points; establish their character (relative minimum, relative maimum, or neither); find intervals

More information

D u f f x h f y k. Applying this theorem a second time, we have. f xx h f yx k h f xy h f yy k k. f xx h 2 2 f xy hk f yy k 2

D u f f x h f y k. Applying this theorem a second time, we have. f xx h f yx k h f xy h f yy k k. f xx h 2 2 f xy hk f yy k 2 93 CHAPTER 4 PARTIAL DERIVATIVES We close this section b giving a proof of the first part of the Second Derivatives Test. Part (b) has a similar proof. PROOF OF THEOREM 3, PART (A) We compute the second-order

More information

Studying the Formation of the Pre-Sheath in an Oblique Magnetic Field using a Fluid Model and PIC Simulation

Studying the Formation of the Pre-Sheath in an Oblique Magnetic Field using a Fluid Model and PIC Simulation J. Plasma Fusion Res. SERIES, Vol. 8 (2009) Studying the Formation of the Pre-Sheath in an Oblique Magnetic Field using a Fluid Model and PIC Simulation Jernej KOVAI 1, Tomaž Gyergyek 2,1, Milan EREK 1,3

More information

Mixed convection boundary layers in the stagnation-point flow toward a stretching vertical sheet

Mixed convection boundary layers in the stagnation-point flow toward a stretching vertical sheet Meccanica (2006) 41:509 518 DOI 10.1007/s11012-006-0009-4 Mied convection boundary layers in the stagnation-point flow toward a stretching vertical sheet A. Ishak R. Nazar I. Pop Received: 17 June 2005

More information

Experimental Study of Impregnation Birch and Aspen Samples

Experimental Study of Impregnation Birch and Aspen Samples Experimental Study of Impregnation Birch and Aspen Samples Igor Vladislavovich Grigorev, a Gleb Vladimirovich Grigorev, a Antonina Ivanovna Nikiforova, a Olga Anatolevna Kunitckaia, a Irina Nikolaevna

More information

MATH 150/GRACEY PRACTICE FINAL. MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question.

MATH 150/GRACEY PRACTICE FINAL. MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. MATH 0/GRACEY PRACTICE FINAL Name MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question. Choose the graph that represents the given function without using

More information

Math 231 Final Exam Review

Math 231 Final Exam Review Math Final Eam Review Find the equation of the line tangent to the curve 4y y at the point (, ) Find the slope of the normal line to y ) ( e at the point (,) dy Find d if cos( y) y 4 y 4 Find the eact

More information

The problem of singularity in impacting systems

The problem of singularity in impacting systems The problem of singularity in impacting systems Soumitro Banerjee, Department of Physics Indian Institute of Science Education & Research, Kolkata, India The problem of singularity in impacting systems

More information

ECE 6341 Spring 2016 HW 2

ECE 6341 Spring 2016 HW 2 ECE 6341 Spring 216 HW 2 Assigned problems: 1-6 9-11 13-15 1) Assume that a TEN models a layered structure where the direction (the direction perpendicular to the layers) is the direction that the transmission

More information

1993 AP Calculus AB: Section I

1993 AP Calculus AB: Section I 99 AP Calculus AB: Section I 9 Minutes Scientific Calculator Notes: () The eact numerical value of the correct answer does not always appear among the choices given. When this happens, select from among

More information

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are:

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are: Curved beams. Introduction Curved beams also called arches were invented about ears ago. he purpose was to form such a structure that would transfer loads, mainl the dead weight, to the ground b the elements

More information

Machine Learning Basics III

Machine Learning Basics III Machine Learning Basics III Benjamin Roth CIS LMU München Benjamin Roth (CIS LMU München) Machine Learning Basics III 1 / 62 Outline 1 Classification Logistic Regression 2 Gradient Based Optimization Gradient

More information

2. Modeling of shrinkage during first drying period

2. Modeling of shrinkage during first drying period 2. Modeling of shrinkage during first drying period In this chapter we propose and develop a mathematical model of to describe nonuniform shrinkage of porous medium during drying starting with several

More information

Notes for Introduction to Partial Di erential Equations, Fall 2018

Notes for Introduction to Partial Di erential Equations, Fall 2018 Notes for Introduction to Partial Di erential Equations, Fall 2018 Esteban G. Tabak 1 Tra c Flow We eplore a simple mathematical model for tra c flow. This will be our introduction to systems of conservation

More information

Fair Game Review. Chapter 8. Graph the linear equation. Big Ideas Math Algebra Record and Practice Journal

Fair Game Review. Chapter 8. Graph the linear equation. Big Ideas Math Algebra Record and Practice Journal Name Date Chapter Graph the linear equation. Fair Game Review. =. = +. =. =. = +. = + Copright Big Ideas Learning, LLC Big Ideas Math Algebra Name Date Chapter Fair Game Review (continued) Evaluate the

More information

x f(x)

x f(x) CALCULATOR SECTION. For y + y = 8 find d point (, ) on the curve. A. B. C. D. dy at the 7 E. 6. Suppose silver is being etracted from a.t mine at a rate given by A'( t) = e, A(t) is measured in tons of

More information