MODELING AND MEASUREMENT OF INTERFACIAL AREA CONCENTRATION IN TWO-PHASE FLOW. Mamoru Ishii and Takashi Hibiki

Size: px
Start display at page:

Download "MODELING AND MEASUREMENT OF INTERFACIAL AREA CONCENTRATION IN TWO-PHASE FLOW. Mamoru Ishii and Takashi Hibiki"

Transcription

1 MODELING AND MEASUREMEN OF INERFACIAL AREA CONCENRAION IN WO-PASE FLOW Mamoru Ishii and akashi ibiki School o Nuclear Enineerin, Purdue University 4 Central Drive, West Laayette, IN , USA ishii@purdue.edu and hibiki@purdue.edu ABSRAC his paper presents experimental and modelin approaches in characterizin interacial structures in as-liquid two-phase low. For the modelin o the interacial structure characterization, the interacial area transport equation proposed earlier has been studied to provide a dynamic and mechanistic prediction tool or two-phase low analysis. A state-o-the-art our-sensor conductivity probe technique has been developed to obtain detailed local interacial structure inormation in a wide rane o low reimes spannin rom bubbly to churn-turbulent lows. Newly obtained interacial area data in 8 8 rod bundle test section are also presented. his paper also reviews available models o the interacial area sink and source terms and existin databases. he interacial area transport equation has been benchmarked usin condensation bubbly low data. 1. INRODUCION In the present state-o-the-art, the two-luid model is the most detailed and accurate macroscopic ormulation o the thermo-luid dynamics o two-phase systems (Ishii, 1975; Ishii and ibiki, 5). he existence o the interacial transer terms is one o the most important characteristics o the twoluid model ormulation. hese terms determine the rate o phase chanes and the deree o mechanical and thermal non-equilibrium between phases, thus they are the essential closure relations which should be modeled accurately. he present thermal-hydraulic system analysis codes such as RELAP5, RAC, and CAARE use one-dimensional orm o the two-luid model equations, where the interacial area concentration is speciied by empirical correlations based on steady-state, ully developed conditions. his approach suers ollowin shortcomins: 1) Durin relatively ast transients, where the relaxation time or the development o the low structure is similar or reater than the characteristic time o the transient itsel, the dynamic nature o the transient cannot be accurately predicted. Analysis o developin lows also suers the same drawback. ) he correlations or interacial area concentration are based on low reimes which are in turn speciied by constitutive equations as discrete unctions o local supericial velocities o two phases. he compound errors in this approach are lare. his also leads to artiicial discontinuities and numerical instabilities in the numerical solutions o the ield equations. 3) he low reime transition criteria and correspondin interacial area concentration correlations have a limited rane o applicability in terms o boundary conditions, luid properties, low eometry and scale. o overcome these problems, the interacial area concentration should be speciied by a transport equation which models the evolution o the eometric structure considerin the physical mechanisms o local interactions between the two phases (Ishii, 1975; Ishii and ibiki, 5). he transport equation can capture the dynamic chanes in the low structure, especially the transitions amon low reimes. ence the transport equation can be used or systems with wide rane o scales and boundary conditions. Followin this introduction, this paper presents the basic idea behind the derivation o the interacial area transport equation and discusses the two-roup approach includin modiied two- 1

2 roup as momentum equation. Furthermore, the measurement technique and the available experimental data are summarized, and newly obtained data in 8 8 rod bundle test section are also presented. Finally, the evaluation o the interacial area transport equation with respect to the database is discussed.. FORMULAION OF INERFACIAL AREA RANSPOR EQUAION.1 wo-roup interacial area transport equation he Boltzmann transport equation describes particle transport by an intero-dierential equation o the particle-distribution unction. Since the interacial area o the luid particle is closely related to the particle number, the interacial area transport equation can be ormulated based on the Boltzmann transport equation (Ishii and ibiki, 5). In a as-liquid two-phase low system, a wide rane o bubble shapes and sizes exist dependin on the iven low reime. hereore, to develop the interacial area transport equation describin the bubble transport in a wide rane o two-phase low reimes, the model must take account o the dierences in the transport characteristics o dierent types o bubbles. hese variations in shape and size o bubbles cause substantial dierences in their transport mechanisms due to the dra orces as well as the bubble interaction mechanisms. In the two-roup ormulation, the bubbles are treated in two roups, namely roup-1 bubbles consistin o spherical and distorted bubbles and roup- bubbles consistin o cap, aylor and churnturbulent bubbles. he roup-1 bubbles exist in the rane o minimum bubble size to maximum distorted bubble size limit, D d,max, whereas the roup- bubbles exist in the rane o D d,max to maximum stable bubble size limit, D max. he boundary bubble sizes, D d,max and D max are iven by σ σ (1) D d,max = 4 and D max = 4, Δρ Δρ where σ : surace tension, : ravitational acceleration, Δρ : density dierence. he two-roup interacial area transport equation can be obtained by averain the interacial area transport equation over the volume rane o each bubble roup as ai1 a i1 α 1 () + ( ai1vi1) = + ( α1v1) η ph 3 α 1 D Vc sc a α i1 1 χ ( α1 1) ηph S S ph AdV i D + v + + V Sm1 α 1, min ai ai α + ( aivi) = + ( αv) 3 α D V sc a α i1 1 max + χ ( α1 1) η ph SAdV i D + v + Vc Sm1 α 1, where a i : interacial area concentration, v i : interacial velocity, α: void raction, t : time, v : as-phase center o mass velocity, η ph : rate o volume enerated by nucleation source per unit mixture volume, χ: coeicient accountin or the contribution rom the inter-roup transer, D sc : surace equivalent diameter o a luid particle with surace area, A i, D Sm : Sauter mean diameter, S and S ph : particle source and sink rates per unit mixture volume due to -th particle interactions and that due to phase chane, respectively, V min, V c and V max : volumes o minimum bubble, critical bubble and maximum bubble, respectively. he two-roup interacial area transport equation is simpliied to a one-roup interacial area transport equation in the bubbly low reime.

3 . wo-roup momentum equation he two-luid model should be modiied or the two-roup interacial area transport equation (Ishii and ibiki, 5). In eneral, the pressure and temperature or roup-1 and roup- bubbles can be assumed to be approximately the same. owever, the velocities o two roups o bubbles are not the same, thereore it is necessary to introduce two continuity and two momentum equations in principle. Based on the above assumption, the density o the as phase is the same or roup-1 and roup- bubbles. he continuity equation or roup-1 and - bubbles are thereore iven by ( α ρ) (3) 1 + ( α ρv ) = Γ Δm , ( αρ) + ( α ρv ) = Γ + Δm 1, where ρ : as density, Γ : mass eneration or as phase, Δm 1 : inter-roup mass transer due to hydrodynamic mechanisms. he momentum equation or roup-1 and - bubbles are iven by ( α ρv ) (4) 1 1 μ + ( α ρ ) α p α ( ) 1 v 1v 1 = α ρ + Γ Δm v α + M + p p α ( ) ( ) i1 1 i1 i1 i1 1 1, ( α ρ v ) μ ( α ρ ) α p α ( ) v v ( m ) ( p p ) + = α ρ + Γ +Δ v α + M + α 1 i i i i, where p : pressure, μ : viscous stress, : turbulent stress, M i : eneralized interacial dra..3 One-dimensional interacial area transport equation he simplest orm o the interacial area transport equation is the one-dimensional ormulation obtained by applyin cross-sectional area averain over Eq.(). he exact mathematical expressions or the area-averaed source and sink terms involve many covariances that may urther complicate the one-dimensional problem. In the current one-dimensional ormulation or adiabatic two-phase low, the covariance terms are nelected because o relatively uniorm low parameter distribution over the low channel. For example, the one-dimensional one-roup interacial area transport equation is expressed as ai a i α (5) + ( ai vi ) = ( ΦB ΦC ) + a { + ( α v ) 3 }, z α z where : area-averaed quantity, a : interacial area concentration-weihted mean quantity, : void raction-weihted mean quantity, Φ B and Φ C : rates o chane o interacial area concentration due to bubble breakup and coalescence, respectively. owever, or subcooled boilin low, the phase distribution pattern may not be assumed uniorm, resultin in many covariances in the one-dimensional interacial area transport equation. o avoid the covariances, a simple model can be introduced to ormulate the transport equation or subcooled boilin low (ibiki et al., 3). In this case, the bubbles mainly exist near a heated wall, whereas almost no bubbles exist ar rom the heated wall. hereore, the low path may be divided into two reions, namely (i) boilin two-phase (bubble layer) reion where the void raction proile can be assumed to be uniorm, and (ii) liquid sinle-phase reion where the void raction can be assumed to be zero. hus, the one-dimensional interacial area transport equation can be obtained by averain the interacial area transport equation over the bubble-layer reion and applyin a actor o AB A C 3

4 to the interacial area concentration in the bubble-layer reion. ere A B and A C are the area o the bubble-layer reion and the cross-sectional area o the boilin channel, respectively. 3. MEASUREMEN ECNIQUE he local time-averaed interacial area concentration can be measured usin our-sensor conductivity probe method (Kataoka et al., 1986) based on the dierence in conductivity between the two phases. he probe is composed o a sensor and an electrically conductive casin. Usin the casin as the common round, the characteristic rise and all o the impedance sinals can be obtained when an interace passes throuh the probe sensor. With the acquired sinals rom the sensor, the local time-averaed void raction can be easily obtained by dividin the sum o the time raction occupied by the as phase by the total measurement time. One o the most important eatures o the conductivity probe is that it can measure the local interacial velocity with multiple sensors. his is o reat importance because the local time-averaed interacial area concentration can be obtained rom the interacial velocity throuh the mathematical relation. he our-sensor conductivity probe is made o our sensors. With one common upstream sensor and three independent downstream sensors, three directional velocities at a local point can be obtained by measurin the time delay between the sinals rom three pairs o double-sensors. When the directions o the three independent probes are chosen, the equation or the time-averaed interacial area concentration can be simpliied as (Kataoka et al., 1986), (6) a i =, Ω + + v s1 v s v s3 where Ω : time interval, v sk : passin velocity o the -th interace over probe k. In Eq.(6), no hypothesis or bubble shape is needed or calculatin the local interacial area concentration rom the interacial velocity. hereore, the our-sensor probe can be utilized in a wide rane o two-phase low reimes where bubbles are no loner spherical in shape. I we consider spherical bubbly low with no correlation between bubble velocity and movin direction, Eq.(6) can be siniicantly simpliied to enable double sensor probe method to measure the interacial area concentration (Kataoka et al., 1986; ibiki et al., 1998). o minimize the inite probe size eect on the measurement, a miniaturized our-sensor conductivity probe has been developed (Kim et al., ). A schematic diaram o the probe desin and its eometrical coniuration is shown in Fi.1. One o the important eatures o the probe desin is that the our sensor probe accommodates a built-in double-sensor probe or measurin small bubbles. hereore, the probe is applicable to a wide rane o low reimes, spannin rom bubbly ~5 mm ~5-7 mm Epoxy and conductive ink Stainless-steel tubin Epoxy Stainless-steel tubin, OD: ~3 mm hermocouple wires Coated sensor body < 5-micron ~.5 mm Sensor tip (uncoated) 1 Not scaled 3 ~.5-.8 mm Fi.1: Coniuration o the our-sensor conductivity probe (Kim et al., ). 4

5 to churn-turbulent low reimes. Alon with the probe desin, the sinal processin is constructed, such that it can identiy and separate the local parameters into two roups, namely: roup-1 or spherical and distorted bubbles and roup- or slu and churn-turbulent bubbles. hrouhout the benchmark experiments, very ew missin interaces are observed or the roup- bubbles unless the probe is traversed very close to the wall o the low duct. he measurement area o the our-sensor probe used in the experiments is less than. mm and the tip distance o the double-sensor probe or small bubbles is.4 mm. his allows the measurable bubble diameter to be as smal1 as 1 mm. he diameter o the sensor electrode is.13 mm, however, the sensor itsel has a diameter o less than.5 mm. he details o the double sensor and our-sensor probe techniques can be ound in ibiki et al. (1998) and Kim et al. (), respectively. 4. DAABASE OF INERFACIAL AREA CONCENRAION 4.1 Existin database Extensive data o axial development o low parameters in adiabatic and boilin two-phase low have been obtained over a wide rane o low conditions includin downward low. he measured low parameters include local void raction, interacial area concentration, interacial velocity, bubble Sauter mean diameter, liquid velocity and liquid turbulence. he covered experimental conditions are est section eometry: Round pipe, conined channel, annulus and rod bundle, est section size: 1 mm to 1 mm, Flow reime: Bubbly, cap-bubbly, slu and churn-turbulent lows, Flow condition: Supericial as velocity,, up to 1 m/s and supericial liquid velocity,, rom -3.1 m/s (i.e. downward low) to 5. m/s (i.e. upward low), Flow direction: Vertical upward and downward lows, hermal condition: Adiabatic and diabatic lows, Gravity condition: Normal and micro ravity conditions, Pressure condition: Atmospheric pressure he extensive review o the existin database can be ound in ibiki and Ishii (1, ) and ibiki et al. (6). In what ollows, newly obtained data taken in 8 8 rod bundle test section are shown. 4. Database or 8 8 rod bundle eometry Recently, axial developments o local low parameters in air-water two-phase low were measured in 8 8 rod bundle test acility. he test section consisted o a 3m lon vertical low channel with square cross section havin sides o lenth 14 mm. It housed an 8 8 array o 64 rods each havin a diameter o 1.7mm arraned at a pitch distance o 16.7 mm. he rods were held in place by six spacer rids located at zd = 31, 61, 91, 11, 151 and 18 where D : hydraulic diameter o a typical subchannel (=14.8 mm), z : axial distance rom the inlet o the test section. he narrowest and widest aps in the center subchannel were, respectively, 4. mm and 1.9 mm. he measurement ports were located at the axial distances o zd =7, 86, 94, 116, 14, 137 and. he detailed inormation on the experimental acility and instrumentation can be ound in Paranape et al. (8). Fiure shows the measurement rid or local low data. At each axial location in the low channel, the local low data were taken at the center o the sub-channels and the narrowest ap between the rods. he local data were taken in 5 axial locations in the low channel under supericial as and liquid velocity conditions which covered bubbly, cap bubbly, cap-turbulent and churn-turbulent low reimes. Fiure 3 shows low visualization in various low reimes. 5

6 d W S x Subchannel Center Rod Gap Center Fi.: Measurement rid in a rod bundle eometry. (a) bubbly low =. m/s, =. m/s. (b) cap bubbly low =.14 m/s, =. m/s. (c) Cap turbulent low (d) Churn turbulent low =.8 m/s, =.1 m/s. = 8.8 m/s, =. m/s. Fi.3: Flow visualization in various low reimes (Paranape et al., 8). he representative data at zd = in two bubbly and one cap-turbulent low reime conditions are shown in Fis.4-7. In Fis.4-6, the data are shown alon the center line o the rod bundle rom the bundle center, x. he distance in the iures is normalized by the hal width o the rod bundle casin desinated by W. In Fi.7, the data is also plotted alon the diaonal line o the rod bundle rom the bundle center, d. he distance in the iure is normalized by the hal width o 6

7 the bundle diaonal lenth desinated by S. he low conditions in Fis.4 and 5 are =. m/s and =. m/s, and =. m/s and =1. m/s, respectively, correspondin to bubbly low reime where only roup-1 bubbles are observed. he low condition in Fis.6 and 7 is =.5 m/s and =. m/s, correspondin to cap-turbulent low reime where two roups o bubbles are observed. Comparin Fis.4 and 5, the eect o increased supericial liquid velocity on the spatial distribution and manitude o low parameters can be clariied, whereas the comparison between Fis.4 and 6 provides some insihts on the eect o increased as velocity and low reime transition on the spatial distribution and manitude o low parameters. Open and solid symbols in Fis.4 and 5 indicate local low parameter measured at subchannel center and rod narrowest ap, respectively. As the supericial liquid velocity increases, the bubble size becomes smaller due to bubble breakup and the bubbles tend to mirate toward the rod narrowest ap, which is similar to wall peakin observed in a round pipe test section (ibiki and Ishii, 1999). his can be explained as ollows. he lit orce actin on a bubble is enerally enhanced by increased velocity radient. he increased liquid velocity enhances the as velocity radient between the subchannel center and rod Void Fraction, <α> [-] Location rom Center, x/w [-] Interacial Area Conc., <a i > [m -1 ] Location rom Center, x/w [-] Gas Velocity, <v > [m/s] Location rom Center, x/w [-] Sauter Mean Diameter, <D Sm > [mm] Location rom Center, x/w [-] Fi.4: Local parameter data alon center line in bubbly low at Flow condition: =. m/s and =. m/s. zd =. 7

8 Void Fraction, <α> [-] Location rom Center, x/w [-] Interacial Area Conc., <a i > [m -1 ] Location rom Center, x/w [-] Gas Velocity, <v > [m/s] Location rom Center, x/w [-] Sauter Mean Diameter, <D Sm > [mm] Location rom Center, x/w [-] Fi.5: Local parameter data alon center-line in bubbly low at zd =. Flow condition: =. m/s and =1. m/s. narrowest ap, which may also indicate the aumented liquid velocity radient. In addition to this, the lit orce direction is lipped over around the bubbles size o 5 mm. I the bubble size is smaller than 5 mm, the lit orce tends to push the bubbles toward a wall. For the bubble size smaller than 5 mm, the absolute value o the lit coeicient decreases with increased bubble size (ibiki and Ishii, 7). hus, the increased supericial liquid velocity decreases the bubble size resultin in the increased absolute value o the lit coeicient. Such combined eects enhance the void raction at the rod narrowest ap. As the bubbles mirate toward the rod narrowest ap, the interacial area concentration near the rod narrowest ap is increased. he as velocity at the subchannel center is hiher than that at the rod narrowest ap, since the liquid velocity is bound to be zero at the rod surace. For the lower liquid velocity condition, the bubble Sauter mean diameter is comparable to the rod narrowest ap (4 mm). Open and solid symbols in Fi.6 indicate local low parameter measured at subchannel center and rod narrowest ap, respectively. Circle and trianle symbols indicate local low parameter or roup-1 and - bubbles. As can be seen rom Fi.6, as the supericial as velocity increases, roup- bubbles, namely cap bubbles are ormed. Unlike the low supericial as velocity condition shown in Fi.5, the dierence in low parameter distribution between the subchannel center and rod narrowest 8

9 Void Fraction, <α> [-] Group at Center Group at Gap Location rom Center, x/w [-] Interacial Area Conc., <a i > [m -1 ] Group at Gap Group at Center Group at Gap Location rom Center, x/w [-] Gas Velocity, <v > [m/s] Group at Center Group at Gap Location rom Center, x/w [-] Sauter Mean Diameter, <D Sm > [mm] Group at Center Group at Gap Location rom Center, x/w [-] Fi.6: Local parameter data alon center-line in cap-turbulent low at Flow condition: =.5 m/s and =. m/s. zd =. ap is insiniicant, which means that the low parameter distribution is inluenced by the presence o the bundle outer casin. Since the size o the roup-1 bubble exceeds 5 mm, the bubbles around the rod narrowest ap may be squeezed by rods. Since lare bubbles tend to rise in the center o the channel, the void raction at the subchannel center becomes hiher. he as velocity shows the power-low distribution over the whole bundle test section in a lobal sense. he as velocity o roup-1 bubble is slihtly hiher than that o roup- bubble. his can be explained by the dierence in dritvelocity in roup-1 and - bubbles. In the tested condition, the Sauter mean diameter o roup- bubble exceeds the hydraulic diameter o the subchannel. Due to the presence o the rods, the drit velocity may be reduced considerably. his can be understood by the act that the drit velocity o a slu bubble is in proportional to the square root o channel diameter. For air-water pipe low at room temperature and atmospheric pressure, the drit velocities or small and slu bubbles becomes equal at D =5.8 mm. In the channel smaller than 5.8 mm, slu bubble risin velocity is smaller than small bubble risin velocity. Fiure 7 shows the local low parameter measured at subchannel center alon the diaonal line o the bundle test section. Interestinly the void raction o roup-1 bubbles has a sliht peak near the bundle outer casin. he distributions o low parameters alon the diaonal line are consistent with those alon the subchannel center line. 9

10 Void Fraction, <α> [-] Group 1 Group Location rom Center, d/s [-] Interacial Area Conc., <a i > [m -1 ] Group 1 Group Location rom Center, d/s [-] Gas Velocity, <v > [m/s] Group 1 Group Location rom Center, d/s [-] Sauter Mean Diameter, <D Sm > [mm] Group 1 Group Location rom Center, d/s [-] Fi.7: Local parameter data alon diaonal line in cap-bubbly low at Flow condition: =.5 m/s and =. m/s. zd =. 5. SINK AND SOURCE ERM MODELING AND EIR EVALUAION o close the interacial area transport equation, extensive eorts to model various sink and source terms o the interacial area transport equation have been made. Maor modeled sink and source terms are summarized in able 1. o demonstrate the capability o the interacial area transport equation, the one-dimensional one-roup interacial area transport equation is evaluated in condensation systems usin ai (7) a v = Φ Φ Φ + α v. i i a I RC CD z 3 α z In Eq.(7), the bubble breakup and coalescence terms are calculated by ibiki and Ishii s model (a), whereas the bulk condensation term is computed by Park et al. model (7). Fiure 8 compares the interacial area transport calculation with condensation data taken in a vertical concentric annulus (Park et al., 7). he low condition is p (inlet pressure) =.13 MPa, (inlet liquid temperature) = 98. C and G (total mass lux) = 139 k/m s (Zeitoun, 1994). As can be seen rom Fi.8, the interacial area concentration chanes due to bubble coalescence, bubble breakup and void raction chane are neliibly small in the tested condition. he condensation in heat transer-controlled reion without bubble number density chane, Φ, is the 1 C

11 maor contribution to the interacial area concentration chane, whereas the contribution o the inertia-controlled reion with bubble number density chane, Φ IC, is about 16.8 %. he interacial area transport equation can predict the interacial area chane alon the low direction successully. able 1: Maor modeled sink and source terms o the interacial area concentration. Cateory Investiator Details One-roup Wu et al. (1998) One-roup bubble coalescence and breakup Bubble ibiki and Ishii (a) One-roup bubble coalescence and breakup Interaction ibiki et al. (1) One-roup bubble coalescence and breakup Yao and Morel (4) One-roup bubble coalescence and breakup wo-roup ibiki and Ishii (b) wo-roup bubble coalescence and breakup Bubble Fu and Ishii (3) wo-roup bubble coalescence and breakup Interaction Sun et al. (4) wo-roup bubble coalescence and breakup Phase Chane Park et al. (7) Bulk condensation Riznic and Ishii (1989) Flushin Wall ibiki and Ishii (3) Active nucleation site density Nucleation Situ et al. (8) Bubble departure size Source Situ et al. (8) Bubbly departure requency IAC Chane, <a i > - <a i > z/d=1 [m -1 ] p =.13 MPa, =98. o C, G=139 k/m s Experimental Data (Zeitoun, 1994) Predicted IAC Chane eat ranser Inertia Void ransport Random Collision urbulent Impact Axial Position, z/d [ - ] Fi.8: Contribution o bubble coalescence, breakup, void transport, and condensation to interacial area transport (Park et al., 7). 6. CONCLUSIONS In relation to the modelin o the interacial transer terms in the two-luid model, the concept o the interacial area transport equation has been proposed to develop a constitutive relation or the interacial area concentration. he interacial area transport equation can replace the traditional low reime maps and reime transition criteria. he chanes in the two-phase low structure can be predicted mechanistically by introducin the interacial area transport equation. he eects o the boundary conditions and low development are eiciently modeled by this transport equation. he successul development o the interacial area transport equation can make a siniicant improvement in the two-luid model ormulation and the prediction accuracy o three-dimensional two-phase low simulations. his paper reviewed the current status o the interacial area transport equation development and presented newly obtained interacial area concentration data in 8 8 rod bundle test acility. Althouh much eorts have been done to develop it, urther modelin and experimental work are required to establish the interacial area transport equation. 11

12 ACKNOWLEDGEMENS his work was perormed under the auspices o the US Nuclear Reulatory Commission and the US Department o Enery. he authors would like to express their sincere appreciation to NRC and DOE stas or their support on this research. he ratitude is also extended to Messrs. S. Paranape and Y. Lian at Purdue University or their help in the bundle experiment. REFERENCES X. Y. Fu, M. Ishii, wo-roup interacial area transport in vertical air-water low I. Mechanistic model, Nucl. En. Des., 19, (3).. ibiki, M. Ishii, Interacial area concentration in steady ully developed bubbly low, Int. J. eat Mass ranser, 44, (1). ibiki, M. Ishii, Experimental study on interacial area transport in bubbly two-phase lows, Int. J. eat Mass ranser, 4, (1999).. ibiki, M. Ishii, One-roup interacial area transport o bubbly lows in vertical round tubes, Int. J. eat Mass ranser, 43, (a).. ibiki, M. Ishii, wo-roup interacial area transport equations at bubbly-to-slu low transition, Nucl. En. Des.,, (b).. ibiki, M., Ishii, Interacial area concentration o bubbly low systems, Chem. En. Sci., 57, ().. ibiki, M. Ishii, Active nucleation site density in boilin systems, Int. J. eat Mass ranser, 46, (3).. ibiki, M. Ishii, Lit orce in bubbly low systems, Chem. En. Sci., 6, (7).. ibiki et al., Local measurement o interacial area, interacial velocity and liquid turbulence in two-phase low, Nucl. En. Des., 184, (1998).. ibiki et al., Interacial area transport o bubbly low in a small diameter pipe, J. Nucl. Sci. echnol., 38, (1).. ibiki et al., Modelin o bubble-layer thickness or ormulation o one-dimensional interacial area transport equation in subcooled boilin two-phase low, Int. J. eat Mass ranser, 46, (3).. ibiki et al., Interacial area concentration in boilin bubbly low systems, Chem. En. Sci., 61, (6). M. Ishii, hermo-luid Dynamic heory o wo-phase Flow, Eyrolles (1975). M. Ishii,. ibiki, hermo-luid Dynamics o wo-phase Flow, Spriner (5). I. Kataoka et al. Local ormulation and measurements o interacial area concentration in two-phase low, Int. J. Multiphase Flow, 1, (1986). S. Kim et al., Development o the miniaturized our-sensor conductivity probe and the sinal processin scheme, Int. J. eat Mass ranser, 43, (). S. Paranape et al., Global low reime identiication in a rod bundle eometry, Proc. ICONE-16, Paper No (8).. S. Park et al., Modelin o the condensation sink term in an interacial area transport equation, Int. J. eat Mass ranser, 5, (7). J. R. Riznic, M. Ishii, Bubble number density and vapor eneration in lashin low, Int. J. eat Mass ranser, 3, (1989). R. Situ et al., Bubble departure requency in orced convective subcooled boilin low, Int. J. eat Mass ranser (8, in print). X. D. Sun et al., Modelin o bubble coalescence and disinteration in conined upward two-phase low, Nucl. En. Des., 3, 3-6 (4). Q. Wu et al., One-roup interacial area transport in vertical bubbly low, Int. J. eat Mass ranser, 41, (1998). W. Yao, C. Morel, Volumetric interacial area prediction in upward bubbly two-phase low, Int. J. eat Mass ranser, 47, (4). O. M. Zeitoun, Subcooled low boilin and condensation, Ph.D. hesis, McMaster University, Canada (1994). 1

Study of In line Tube Bundle Heat Transfer to Downward Foam Flow

Study of In line Tube Bundle Heat Transfer to Downward Foam Flow Proceedins o the 5th IASME/WSEAS Int. Conerence on Heat Transer, Thermal Enineerin and Environment, Athens, Greece, Auust 25-27, 7 167 Study o In line Tube Bundle Heat Transer to Downward Foam Flow J.

More information

Evaporation (Chapter 14) Zan Wu Room: 5123

Evaporation (Chapter 14) Zan Wu Room: 5123 Evaporation (Chapter 14) Zan Wu zan.wu@enery.lth.se Room: 5123 Evaporation, Boilin vätska, liquid 1) Local boilin or subcooled boilin 2) Boilin with net evaporation q Pool boilin Forced convective boilin

More information

INFLUENCE OF TUBE BUNDLE GEOMETRY ON HEAT TRANSFER TO FOAM FLOW

INFLUENCE OF TUBE BUNDLE GEOMETRY ON HEAT TRANSFER TO FOAM FLOW HEFAT7 5 th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics Sun City, South Africa Paper number: GJ1 INFLUENCE OF TUBE BUNDLE GEOMETRY ON HEAT TRANSFER TO FOAM FLOW Gylys

More information

ASSESSMENT OF AN INTERFACIAL SHEAR TERM FOR ADIABATIC DISPERSED AIR-WATER TWO-PHASE FLOW WITH THE TWO-FLUID MODEL

ASSESSMENT OF AN INTERFACIAL SHEAR TERM FOR ADIABATIC DISPERSED AIR-WATER TWO-PHASE FLOW WITH THE TWO-FLUID MODEL ASSESSMEN OF AN INERFACIAL SHEAR ERM FOR ADIABAIC DISPERSED AIR-WAER WO-PHASE FLOW WIH HE WO-FLUID MODEL S. L. Sharma,. Hibii, M. Ishii School o Nuclear Engineering, Purdue University 400 Central Dr.,

More information

Title. Author(s) 尾崎, 哲浩. Issue Date DOI. Doc URL. Type. File Information. Drag Force Models /doctoral.k13343

Title. Author(s) 尾崎, 哲浩. Issue Date DOI. Doc URL. Type. File Information. Drag Force Models /doctoral.k13343 Title Improvement o Accuracy and Reliability on BWR Therm Drag Force Models Author(s) 尾崎, 哲浩 Issue Date 2018-09-25 DOI 10.14943/doctoral.k13343 Doc URL http://hdl.handle.net/2115/71808 Type theses (doctoral)

More information

Thermodynamic wetness loss calculation in a steam turbine rotor tip section: nucleating steam flow

Thermodynamic wetness loss calculation in a steam turbine rotor tip section: nucleating steam flow Journal o Physics: Conerence Series PAPER OPEN ACCESS Thermodynamic wetness loss calculation in a steam turbine rotor tip section: nucleatin steam low To cite this article: Joby Joseph et al 016 J. Phys.:

More information

ANALYSIS OF THE INTERFACIAL AREA TRANSPORT MODEL FOR INDUSTRIAL 2-PHASE BOILING FLOW APPLICATIONS

ANALYSIS OF THE INTERFACIAL AREA TRANSPORT MODEL FOR INDUSTRIAL 2-PHASE BOILING FLOW APPLICATIONS ANALYSIS OF THE INTERFACIAL AREA TRANSPORT MODEL FOR INDUSTRIAL 2-PHASE BOILING FLOW APPLICATIONS K. Goodheart, N. Alleborn, A. Chatelain and T. Keheley AREVA - AREVA GmbH, Postbox 1109, 91001 Erlanen

More information

CORE HEATUP PREDICTION DURING SB LOCA WITH RELAP5/MOD3.2.2 GAMMA

CORE HEATUP PREDICTION DURING SB LOCA WITH RELAP5/MOD3.2.2 GAMMA International Conerence Nuclear Enery in Central Europe Hoteli Bernardin, Portorož, Slovenia, September -, www: http://www.drustvo-js.si/port/ e-mail: PORT@ijs.si tel.:+ 5 57, + 5 5 ax:+ 5 5 Nuclear Society

More information

DEVELOPMENT AND VALIDATION OF A NEW DRIFT FLUX MODEL IN ROD BUNDLE GEOMETRIES

DEVELOPMENT AND VALIDATION OF A NEW DRIFT FLUX MODEL IN ROD BUNDLE GEOMETRIES DEVELOPMENT AND VALIDATION OF A NEW DRIFT FLUX MODEL IN ROD BUNDLE GEOMETRIES Ikuo Kinoshita and Toshihide Torige Institute o Nuclear Saety System, Inc. 64 Sata, Mihama-cho, Mikata-gun, Fukui 99-25, Japan

More information

STRENGTH ESTIMATION OF END FAILURES IN CORRUGATED STEEL SHEAR DIAPHRAGMS

STRENGTH ESTIMATION OF END FAILURES IN CORRUGATED STEEL SHEAR DIAPHRAGMS SDSS Rio STABILITY AND DUCTILITY OF STEEL STRUCTURES Nobutaka Shimizu et al. (Eds.) Rio de Janeiro, Brazil, September 8 -, STRENGTH ESTIMATION OF END FAILURES IN CORRUGATED STEEL SHEAR DIAPHRAGMS Nobutaka

More information

AN ABSTRACT OF THE THESIS OF. Younghoon Kwak for the degree of Doctor of Philosophy in Mechanical Engineering presented on June 19, 2008.

AN ABSTRACT OF THE THESIS OF. Younghoon Kwak for the degree of Doctor of Philosophy in Mechanical Engineering presented on June 19, 2008. AN ABSTRACT OF THE THESIS OF Younhoon Kwak or the deree o Doctor o Philosophy in Mechanical Enineerin presented on June 19, 2008. Title: Experimental Study o Two-Phase Gas-Liquid Flow in a Microscale Fractal-Like

More information

DEVELOPMENT OF INTERFACIAL AREA TRANSPORT EQUATION

DEVELOPMENT OF INTERFACIAL AREA TRANSPORT EQUATION DEVELOPMENT OF INTERFACIAL AREA TRANSPORT EQUATION MAMORU ISHII *, SEUNGJIN KIM 1 and JOSEPH KELLY 2 School of Nuclear Engineering Purdue University 400 Central Drive, West Lafaytte, IN 47907-2017, USA

More information

InterPACKICNMM

InterPACKICNMM Proceedins o the ASME 2015 International Conerence and Exhibition on Packain and Interation o Electronic and Photonic Microsystems and ASME 2015 International Conerence on Nanochannels, Microchannels,

More information

Mixture Behavior, Stability, and Azeotropy

Mixture Behavior, Stability, and Azeotropy 7 Mixture Behavior, Stability, and Azeotropy Copyrihted Material CRC Press/Taylor & Francis 6 BASIC RELATIONS As compounds mix to some deree in the liquid phase, the Gibbs enery o the system decreases

More information

Colloids: Dilute Dispersions and Charged Interfaces

Colloids: Dilute Dispersions and Charged Interfaces 17-9-15 Colloids: Dilute Dispersions and Chared Interaces Andreas B. Dahlin ecture 1/6 Jones: 4.1-4.3, Hamley: 3.1-3.4 adahlin@chalmers.se http://www.adahlin.com/ 17-9-15 Sot Matter Physics 1 Continuous

More information

1. INTRODUCTION. Adrian Tentner 1, Simon Lo 2, David Pointer 1, Andrew Splawski 2

1. INTRODUCTION. Adrian Tentner 1, Simon Lo 2, David Pointer 1, Andrew Splawski 2 ADVANCES IN THE DEVELOPMENT AND VALIDATION OF CFD-BWR, A TWO-PHASE COMPUTATIONAL FLUID DYNAMICS MODEL FOR THE SIMULATION OF FLOW AND HEAT TRANSFER IN BOILING WATER REACTORS Adrian Tentner 1, Simon Lo 2,

More information

Analysis of Non-Thermal Equilibrium in Porous Media

Analysis of Non-Thermal Equilibrium in Porous Media Analysis o Non-Thermal Equilibrium in Porous Media A. Nouri-Borujerdi, M. Nazari 1 School o Mechanical Engineering, Shari University o Technology P.O Box 11365-9567, Tehran, Iran E-mail: anouri@shari.edu

More information

CONVECTIVE HEAT TRANSFER CHARACTERISTICS OF NANOFLUIDS. Convective heat transfer analysis of nanofluid flowing inside a

CONVECTIVE HEAT TRANSFER CHARACTERISTICS OF NANOFLUIDS. Convective heat transfer analysis of nanofluid flowing inside a Chapter 4 CONVECTIVE HEAT TRANSFER CHARACTERISTICS OF NANOFLUIDS Convective heat transer analysis o nanoluid lowing inside a straight tube o circular cross-section under laminar and turbulent conditions

More information

Propagation Modes in Multimode Graded-Index Fibers

Propagation Modes in Multimode Graded-Index Fibers International Journal o Science and Research (IJSR) ISSN (Online): 319-7064 Index Copernicus Value (013): 6.14 Impact Factor (015): 6.391 Propaation Modes in Multie Graded-Index Fibers Zaman Hameed Kareem

More information

SIMULATION OF HEAT TRANSFER THROUGH WOVEN FABRICS BASED ON THE FABRIC GEOMETRY MODEL

SIMULATION OF HEAT TRANSFER THROUGH WOVEN FABRICS BASED ON THE FABRIC GEOMETRY MODEL SIMULATION OF HEAT TRANSFER THROUGH WOVEN FABRICS BASED ON THE FABRIC GEOMETRY MODEL Zhenron Zhen a,b*, Nannan Zhan a and Xiaomin Zhao a,* a Collee o Tetiles, Tianjin Polytechnic University, Tianjin, 300387,

More information

Advanced Methods Development for Equilibrium Cycle Calculations of the RBWR. Andrew Hall 11/7/2013

Advanced Methods Development for Equilibrium Cycle Calculations of the RBWR. Andrew Hall 11/7/2013 Advanced Methods Development for Equilibrium Cycle Calculations of the RBWR Andrew Hall 11/7/2013 Outline RBWR Motivation and Desin Why use Serpent Cross Sections? Modelin the RBWR Axial Discontinuity

More information

Pneumatic Conveying in Horizontal Pipes: Eulerian Modeling and Pressure Drop Characteristics

Pneumatic Conveying in Horizontal Pipes: Eulerian Modeling and Pressure Drop Characteristics American Journal of Mathematical and Computational Sciences 08; (): 0-6 http://www.aascit.or/journal/ajmcs Pneumatic Conveyin in Horizontal Pipes: Eulerian Modelin and Pressure Drop Characteristics Pandaba

More information

1 Introduction. Korea Atomic Energy Research Institute, South Korea.

1 Introduction. Korea Atomic Energy Research Institute, South Korea. Tenth International Conference on Computational Fluid Dynamics (ICCFD10), Barcelona, Spain, July 9-13, 2018 ICCFD10-0206 Multi-physics approach for nuclear reactor analysis usin thermal-hydraulics and

More information

Categories and Quantum Informatics: Monoidal categories

Categories and Quantum Informatics: Monoidal categories Cateories and Quantum Inormatics: Monoidal cateories Chris Heunen Sprin 2018 A monoidal cateory is a cateory equipped with extra data, describin how objects and morphisms can be combined in parallel. This

More information

Controlling the Heat Flux Distribution by Changing the Thickness of Heated Wall

Controlling the Heat Flux Distribution by Changing the Thickness of Heated Wall J. Basic. Appl. Sci. Res., 2(7)7270-7275, 2012 2012, TextRoad Publication ISSN 2090-4304 Journal o Basic and Applied Scientiic Research www.textroad.com Controlling the Heat Flux Distribution by Changing

More information

5. Network Analysis. 5.1 Introduction

5. Network Analysis. 5.1 Introduction 5. Network Analysis 5.1 Introduction With the continued rowth o this country as it enters the next century comes the inevitable increase in the number o vehicles tryin to use the already overtaxed transportation

More information

Effects of Dissipation and Radiation on Heat Transfer Flow of a Convective Rotating Cuo-Water Nano-fluid in a Vertical Channel

Effects of Dissipation and Radiation on Heat Transfer Flow of a Convective Rotating Cuo-Water Nano-fluid in a Vertical Channel 50, Issue 2 (208) 08-7 Journal o Advanced Research in Fluid Mechanics and Thermal Sciences Journal homepae: www.akademiabaru.com/armts.html ISSN: 2289-7879 Eects o Dissipation and Radiation on Heat Transer

More information

Appendix A: Uncertainty Analysis

Appendix A: Uncertainty Analysis Appendix A: Uncertainty Analysis o compute the uncertainty in the experimental data o this work, error analyses have been conducted according to the principles proposed by aylor [1]. he error analysis

More information

ULOF Accident Analysis for 300 MWt Pb-Bi Coolled MOX Fuelled SPINNOR Reactor

ULOF Accident Analysis for 300 MWt Pb-Bi Coolled MOX Fuelled SPINNOR Reactor ULOF Accident Analysis for 300 MWt Pb-Bi Coolled MOX Fuelled SPINNOR Reactor Ade afar Abdullah Electrical Enineerin Department, Faculty of Technoloy and Vocational Education Indonesia University of Education

More information

2.3. PBL Equations for Mean Flow and Their Applications

2.3. PBL Equations for Mean Flow and Their Applications .3. PBL Equations for Mean Flow and Their Applications Read Holton Section 5.3!.3.1. The PBL Momentum Equations We have derived the Reynolds averaed equations in the previous section, and they describe

More information

Altitude measurement for model rocketry

Altitude measurement for model rocketry Altitude measurement for model rocketry David A. Cauhey Sibley School of Mechanical Aerospace Enineerin, Cornell University, Ithaca, New York 14853 I. INTRODUCTION In his book, Rocket Boys, 1 Homer Hickam

More information

Problems of the 9 th International Physics Olympiads (Budapest, Hungary, 1976)

Problems of the 9 th International Physics Olympiads (Budapest, Hungary, 1976) Problems of the 9 th International Physics Olympiads (Budapest, Hunary, 1976) Theoretical problems Problem 1 A hollow sphere of radius R = 0.5 m rotates about a vertical axis throuh its centre with an

More information

Evaluation of the SONAR Meter in Wet Gas Flow for an Offshore Field Development

Evaluation of the SONAR Meter in Wet Gas Flow for an Offshore Field Development Evaluation of the SONAR Meter in Wet Gas Flow for an Offshore Field Development Anela Floyd, BP Siddesh Sridhar and Gabriel Dranea, Expro Meters 1 INTRODUCTION The ABC project is a hih pressure as condensate

More information

On-Line Trajectory Optimization Including Moving Threats and Targets

On-Line Trajectory Optimization Including Moving Threats and Targets AIAA Guidance, Naviation, and Control Conerence and Ehibit 6-9 Auust 00, Providence, Rhode Island AIAA 00-59 On-Line rajector Optimization Includin Movin hreats and arets hannon wi *, Anthon Calise and

More information

International Journal of Heat and Mass Transfer

International Journal of Heat and Mass Transfer International Journal o Heat and Mass Transer 58 (2013) 718 734 Contents lists available at SciVerse ScienceDirect International Journal o Heat and Mass Transer journal homepae: www.elsevier.com/locate/ijhmt

More information

FLOW CHARACTERISTICS OF HFC-134a IN AN ADIABATIC HELICAL CAPILLARY TUBE

FLOW CHARACTERISTICS OF HFC-134a IN AN ADIABATIC HELICAL CAPILLARY TUBE E HEFAT7 5 th International Conerence on Heat Transer, Fluid Mechanics and Thermodynamics Sun City, South Arica Paper number: KM1 FLOW CHARACTERISTICS OF HFC-1a IN AN ADIABATIC HELICAL CAPILLARY TUBE Khan

More information

Numerical Investigation of Downward Continuation Techniques for

Numerical Investigation of Downward Continuation Techniques for Numerical Investiation o Downward Continuation Techniques or Gravity Anomalies J. HUANG, M. G. SIDEIS, P. VANÍČEK 3, I. N. TZIAVOS 4 Geodetic Survey Division, Natural esources Canada, 65 Booth Street,

More information

OE4625 Dredge Pumps and Slurry Transport. Vaclav Matousek October 13, 2004

OE4625 Dredge Pumps and Slurry Transport. Vaclav Matousek October 13, 2004 OE465 Vaclav Matousek October 13, 004 1 Dredge Vermelding Pumps onderdeel and Slurry organisatie Transport OE465 Vaclav Matousek October 13, 004 Dredge Vermelding Pumps onderdeel and Slurry organisatie

More information

SECTION A Torque and Statics

SECTION A Torque and Statics AP Physics C Multiple Choice Practice Rotation SECTON A Torque and Statics 1. A square piece o plywood on a horizontal tabletop is subjected to the two horizontal orces shown above. Where should a third

More information

Slip-Flow and Heat Transfer in Isoflux Rectangular Microchannels with Thermal Creep Effects

Slip-Flow and Heat Transfer in Isoflux Rectangular Microchannels with Thermal Creep Effects Journal of Applied Fluid Mechanics, Vol. 3, No. 2, pp. 33-4, 200. Available online at www.jafmonline.net, ISSN 735-3645. Slip-Flow and Heat Transfer in Isoflux Rectanular Microchannels with Thermal Creep

More information

Model to predict the mechanical behaviour of oriented rigid PVC

Model to predict the mechanical behaviour of oriented rigid PVC Louhborouh University Institutional Repository Model to predict the mechanical behaviour o oriented riid PVC This item was submitted to Louhborouh University's Institutional Repository by the/an author.

More information

ADS-IRWST Transient Evaluation Model for AP1000 SBLOCA Analysis. Han Wang 1, Peipei Chen *2

ADS-IRWST Transient Evaluation Model for AP1000 SBLOCA Analysis. Han Wang 1, Peipei Chen *2 ADS-IRWST Transient Evaluation Model for AP1000 SBLOCA Analysis Han Wan 1, Peipei Chen * 1. State Nuclear Power Technoloy R&D Center Future S&T City, Chanpin, Beijin, China. State Nuclear Power Technoloy

More information

Physics 111 P 2 A = P 1. A + mg = P 1. A + ρ( AΔh)g. Wednesday, 8-9 pm in NSC 118/119 Sunday, 6:30-8 pm in CCLIR 468.

Physics 111 P 2 A = P 1. A + mg = P 1. A + ρ( AΔh)g. Wednesday, 8-9 pm in NSC 118/119 Sunday, 6:30-8 pm in CCLIR 468. ics Announcements day, ember 11, 011 C5: Fluids Pascal s Principle Archimede s Principle Fluid Flows Continuity Equation Bernoulli s Equation Toricelli s Theorem Wednesday, 8-9 pm in NSC 118/119 Sunday,

More information

Investigation of ternary systems

Investigation of ternary systems Investiation of ternary systems Introduction The three component or ternary systems raise not only interestin theoretical issues, but also have reat practical sinificance, such as metallury, plastic industry

More information

Exam 2A Solution. 1. A baseball is thrown vertically upward and feels no air resistance. As it is rising

Exam 2A Solution. 1. A baseball is thrown vertically upward and feels no air resistance. As it is rising Exam 2A Solution 1. A baseball is thrown vertically upward and feels no air resistance. As it is risin Solution: Possible answers: A) both its momentum and its mechanical enery are conserved - incorrect.

More information

(A) (B) (C) (D) None of these

(A) (B) (C) (D) None of these Exercise OBJECTIVE PROBLEMS. Action and reaction (A) act on two different objects (C) have opposite directions. Which fiure represents the correct F.B.D. of rod of mass m as shown in fiure : (B) have equal

More information

Homework # 2. SOLUTION - We start writing Newton s second law for x and y components: F x = 0, (1) F y = mg (2) x (t) = 0 v x (t) = v 0x (3)

Homework # 2. SOLUTION - We start writing Newton s second law for x and y components: F x = 0, (1) F y = mg (2) x (t) = 0 v x (t) = v 0x (3) Physics 411 Homework # Due:..18 Mechanics I 1. A projectile is fired from the oriin of a coordinate system, in the x-y plane (x is the horizontal displacement; y, the vertical with initial velocity v =

More information

Gas-side mass transfer coefficient of a laboratory column equipped with one sieve tray

Gas-side mass transfer coefficient of a laboratory column equipped with one sieve tray Gas-side mass transer coeicient o a laoratory column equipped with one sieve tray Zhivko Ivanov, Zhelcho Steanov, Bogdan Bogdanov Astract: The inluence o plate geometry on the characteristics o luid low

More information

HEAT TRANSFER IN EXHAUST SYSTEM OF A COLD START ENGINE AT LOW ENVIRONMENTAL TEMPERATURE

HEAT TRANSFER IN EXHAUST SYSTEM OF A COLD START ENGINE AT LOW ENVIRONMENTAL TEMPERATURE THERMAL SCIENCE: Vol. 14 (2010) Suppl. pp. S219 S232 219 HEAT TRANSFER IN EXHAUST SYSTEM OF A COLD START ENGINE AT LOW ENVIRONMENTAL TEMPERATURE by Snežana D. PETKOVIĆ a Radivoje B. PEŠIĆ b b and Jovanka

More information

Recursive Credibility: Using Credibility to Blend Reserve Assumptions

Recursive Credibility: Using Credibility to Blend Reserve Assumptions Recursive Credibility: Usin Credibility to Blend Reserve Assumptions by Marcus M. Yamashiro ABSTRACT When estimatin loss reserves, actuaries usually ive varyin weihts to multiple indications to arrive

More information

Multiphase Flow and Heat Transfer

Multiphase Flow and Heat Transfer Multiphase Flow and Heat Transfer ME546 -Sudheer Siddapureddy sudheer@iitp.ac.in Two Phase Flow Reference: S. Mostafa Ghiaasiaan, Two-Phase Flow, Boiling and Condensation, Cambridge University Press. http://dx.doi.org/10.1017/cbo9780511619410

More information

MODELING WELLBORE PRESSURE WITH APPLICATION TO MULTI-STAGE, ACID-STIMULATION TREATMENT

MODELING WELLBORE PRESSURE WITH APPLICATION TO MULTI-STAGE, ACID-STIMULATION TREATMENT MODELING WELLBORE PRESSURE WITH APPLICATION TO MULTI-STAGE, ACID-STIMULATION TREATMENT A Thesis by EFEJERA A. EJOFODOMI Submitted to the Oice o Graduate Studies o Texas A&M University in partial ulillment

More information

A Critical Investigation of High-Order Flux Limiters In Multiphase Flow Problems

A Critical Investigation of High-Order Flux Limiters In Multiphase Flow Problems A Critical Investigation o High-Order Flux Limiters In Multiphase Flow Problems Chris Guenther Fluent In., 3647 Collins Ferry Rd., Morgantown, WV 26505, USA cpg@luent.com ABSTRACT. In recent years inite

More information

1. Introduction. ) exceeded the terminal velocity (U t

1. Introduction. ) exceeded the terminal velocity (U t Excerpt from the Proceedins of the COMOL Conference 010 India Cluster Diameter Determination of Gas-solid Dispersed Particles in a Fluidized Bed Reactor *Mitali Das Department of Biotechnoloy, PEIT Banalore

More information

THE NEAR-WELLBORE PRESSURE CALCULATION MODEL INCORPORATING THERMOCHEMICAL EFFECT

THE NEAR-WELLBORE PRESSURE CALCULATION MODEL INCORPORATING THERMOCHEMICAL EFFECT HERMAL CIENCE: Year 2018, Vol. 22, No. 1B, pp. 623-630 623 HE NEAR-WELLBORE PREURE CALCULAION MODEL INCORPORAING HERMOCHEMICAL EFFEC by Zhiqiang ANG, Qian LI *, and Hu YIN Petroleum and Natural Gas Engineering

More information

OVERTURNING CRITERIA FOR FREE-STANDING RIGID BLOCKS TO EARTHQUAKE PULSES

OVERTURNING CRITERIA FOR FREE-STANDING RIGID BLOCKS TO EARTHQUAKE PULSES 0 th HSTAM International Conress on Mechanics Chania, Crete, Greece, 5 7 May, 03 OVERTURNING CRITERIA FOR FREE-STANDING RIGID BLOCKS TO EARTHQUAKE PULSES Elia Voyaaki, Ioannis N. Psycharis and Geore E.

More information

3D Numerical Modelling of Convective Heat Transfer through Two-sided Vertical Channel Symmetrically Filled with Metal Foams

3D Numerical Modelling of Convective Heat Transfer through Two-sided Vertical Channel Symmetrically Filled with Metal Foams P Periodica Polytechnica Mechanical Engineering P 60(4), pp. 193-202, 2016 DOI: 10.3311/PPme.8511 Creative Commons Attribution b 3D Numerical Modelling o Convective Heat Transer through Two-sided Vertical

More information

Investigation of Initial Fouling Rates of Calcium Sulfate Solutions under Non-Boiling Conditions (Work-in-Progress)

Investigation of Initial Fouling Rates of Calcium Sulfate Solutions under Non-Boiling Conditions (Work-in-Progress) eereed Proceedings Heat Exchanger Fouling and Cleaning: Fundamentals and Applications Engineering Conerences International Year 23 Investigation o Initial Fouling ates o Calcium Sulate Solutions under

More information

INFLUENCE OF PROPELLER PRESENCE AND CAVITATION ON LIQUID NUCLEI POPULATION

INFLUENCE OF PROPELLER PRESENCE AND CAVITATION ON LIQUID NUCLEI POPULATION 7 th International Symposium on Cavitation CAV2009 Auust 16-22, 2009, Ann Harbor, Michian, USA INFLUENCE OF PROPELLER PRESENCE AND CAVITATION ON LIQUID NUCLEI POPULATION Reni Raju DYNAFLOW INC. Jessup,

More information

Chapter 8 Applications of Newton s Second Law

Chapter 8 Applications of Newton s Second Law 81 Force Laws 2 Chapter 8 Applications of Newton s Second Law 811 Hooke s Law 2 822 Principle of Equivalence: 6 823 Gravitational Force near the Surface of the Earth 7 824 Electric Chare and Coulomb s

More information

Modeling for control of a three degrees-of-freedom Magnetic. Levitation System

Modeling for control of a three degrees-of-freedom Magnetic. Levitation System Modelin for control of a three derees-of-freedom Manetic evitation System Rafael Becerril-Arreola Dept. of Electrical and Computer En. University of Toronto Manfredi Maiore Dept. of Electrical and Computer

More information

Experiment 1: Simple Pendulum

Experiment 1: Simple Pendulum COMSATS Institute of Information Technoloy, Islamabad Campus PHY-108 : Physics Lab 1 (Mechanics of Particles) Experiment 1: Simple Pendulum A simple pendulum consists of a small object (known as the bob)

More information

Expanded Knowledge on Orifice Meter Response to Wet Gas Flows

Expanded Knowledge on Orifice Meter Response to Wet Gas Flows 32 nd International North Sea Flow Measurement Workshop 21-24 October 2014 Expanded Knowlede on Orifice Meter Response to Wet Gas Flows Richard Steven, Colorado Enineerin Experiment Station Inc Josh Kinney,

More information

Design of Chevron Gusset Plates

Design of Chevron Gusset Plates 017 SEAOC CONENTION PROCEEDINGS Desin of Chevron Gusset Plates Rafael Sali, Director of Seismic Desin Walter P Moore San Francisco, California Leih Arber, Senior Enineer American Institute of Steel Construction

More information

A Mathematical Model for the Fire-extinguishing Rocket Flight in a Turbulent Atmosphere

A Mathematical Model for the Fire-extinguishing Rocket Flight in a Turbulent Atmosphere A Mathematical Model for the Fire-extinuishin Rocket Fliht in a Turbulent Atmosphere CRISTINA MIHAILESCU Electromecanica Ploiesti SA Soseaua Ploiesti-Tiroviste, Km 8 ROMANIA crismihailescu@yahoo.com http://www.elmec.ro

More information

Categorical Background (Lecture 2)

Categorical Background (Lecture 2) Cateorical Backround (Lecture 2) February 2, 2011 In the last lecture, we stated the main theorem o simply-connected surery (at least or maniolds o dimension 4m), which hihlihts the importance o the sinature

More information

Development of Crane Tele-operation System using Laser Pointer Interface

Development of Crane Tele-operation System using Laser Pointer Interface 23 IEEE/RSJ International Conerence on Intellient Robots and Systems (IROS) November 3-7, 23. Tokyo, Japan Development o Crane Tele-operation System usin Laser Pointer Interace Masaki Neishi, Hisasi Osumi

More information

ONLINE: MATHEMATICS EXTENSION 2 Topic 6 MECHANICS 6.3 HARMONIC MOTION

ONLINE: MATHEMATICS EXTENSION 2 Topic 6 MECHANICS 6.3 HARMONIC MOTION ONINE: MATHEMATICS EXTENSION Topic 6 MECHANICS 6.3 HARMONIC MOTION Vibrations or oscillations are motions that repeated more or less reularly in time. The topic is very broad and diverse and covers phenomena

More information

Ultra Fast Calculation of Temperature Profiles of VLSI ICs in Thermal Packages Considering Parameter Variations

Ultra Fast Calculation of Temperature Profiles of VLSI ICs in Thermal Packages Considering Parameter Variations Ultra Fast Calculation o Temperature Proiles o VLSI ICs in Thermal Packages Considering Parameter Variations Je-Hyoung Park, Virginia Martín Hériz, Ali Shakouri, and Sung-Mo Kang Dept. o Electrical Engineering,

More information

Experimental and Computational Studies of Gas Mixing in Conical Spouted Beds

Experimental and Computational Studies of Gas Mixing in Conical Spouted Beds Refereed Proceedins The 1th International Conference on Fluidization - New Horizons in Fluidization Enineerin Enineerin Conferences International Year 007 Experimental and Computational Studies of Gas

More information

The Measurement of the Gravitational Constant g with Kater s Pendulum

The Measurement of the Gravitational Constant g with Kater s Pendulum e Measurement of te Gravitational Constant wit Kater s Pendulum Abstract A Kater s pendulum is set up to measure te period of oscillation usin a lamppotocell module and a ektronix oscilloscope. Usin repeated

More information

Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science

Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science Massachusetts nstitute of Technoloy Department of Electrical Enineerin and Computer Science 6.685 Electric Machines Class Notes 2 Manetic Circuit Basics September 5, 2005 c 2003 James L. Kirtley Jr. 1

More information

ANALYZE In all three cases (a) (c), the reading on the scale is. w = mg = (11.0 kg) (9.8 m/s 2 ) = 108 N.

ANALYZE In all three cases (a) (c), the reading on the scale is. w = mg = (11.0 kg) (9.8 m/s 2 ) = 108 N. Chapter 5 1. We are only concerned with horizontal forces in this problem (ravity plays no direct role). We take East as the +x direction and North as +y. This calculation is efficiently implemented on

More information

Electromagnetic Time Reversal Applied to Fault Location: On the Properties of Back-Injected Signals

Electromagnetic Time Reversal Applied to Fault Location: On the Properties of Back-Injected Signals Electromanetic Time Reversal Applied to Fault Location: On the Properties o Back-Injected Sinals Zhaoyan Wan, Reza Razzahi, Mario Paolone, and Farhad Rachidi Electromanetic Compatibility (EMC) Laboratory,

More information

The Ideal thermodynamic cycle for gas liquefaction is impractical and hence modified cycles are proposed.

The Ideal thermodynamic cycle for gas liquefaction is impractical and hence modified cycles are proposed. Earlier Lecture The Ideal thermodynamic cycle or as liqueaction is impractical and hence modiied cycles are proposed. An Ideal cycle is used as a benchmark and in eect, dierent ratios and unctions are

More information

Chapter 6 Reliability-based design and code developments

Chapter 6 Reliability-based design and code developments Chapter 6 Reliability-based design and code developments 6. General Reliability technology has become a powerul tool or the design engineer and is widely employed in practice. Structural reliability analysis

More information

Fluid Mechanics (ME 201) 1

Fluid Mechanics (ME 201) 1 Fluid Mechanics (ME 201) 1 9 Forces on Submered Bodies 9.1 Net Force on a Submered Plane Surfaces In this section, we will compute the forces actin on a plane surface. We consider a surface oriented at

More information

Generation of random waves in time-dependent extended mild-slope. equations using a source function method

Generation of random waves in time-dependent extended mild-slope. equations using a source function method Generation of random waves in time-dependent etended mild-slope equations usin a source function method Gunwoo Kim a, Chanhoon Lee b*, Kyun-Duck Suh c a School of Civil, Urban, and Geosystem Enineerin,

More information

Prediction of Well Bore Temperatures during Ultra-Deep Drilling

Prediction of Well Bore Temperatures during Ultra-Deep Drilling Prediction o Well Bore Temperatures during Ultra-Deep Drilling Fanhe Meng, Aiguo Yao*, Shuwei Dong Faculty o Engineering China University o Geosciences Wuhan, Hubei, 430074, China Abstract In order to

More information

Buoyancy Driven Heat Transfer of Water-Based CuO Nanofluids in a Tilted Enclosure with a Heat Conducting Solid Cylinder on its Center

Buoyancy Driven Heat Transfer of Water-Based CuO Nanofluids in a Tilted Enclosure with a Heat Conducting Solid Cylinder on its Center July 4-6 2012 London U.K. Buoyancy Driven Heat Transer o Water-Based CuO Nanoluids in a Tilted Enclosure with a Heat Conducting Solid Cylinder on its Center Ahmet Cihan Kamil Kahveci and Çiğdem Susantez

More information

Application of System Codes to Void Fraction Prediction in Heated Vertical Subchannels

Application of System Codes to Void Fraction Prediction in Heated Vertical Subchannels Application of System Codes to Void Fraction Prediction in Heated Vertical Subchannels Taewan Kim Incheon National University, 119 Academy-ro, Yeonsu-gu, Incheon 22012, Republic of Korea. Orcid: 0000-0001-9449-7502

More information

A Semi-Analytical Solution for a Porous Channel Flow of a Non-Newtonian Fluid

A Semi-Analytical Solution for a Porous Channel Flow of a Non-Newtonian Fluid Journal o Applied Fluid Mechanics, Vol. 9, No. 6, pp. 77-76, 6. Available online at www.jamonline.net, ISSN 735-357, EISSN 735-3645. A Semi-Analytical Solution or a Porous Channel Flow o a Non-Newtonian

More information

Get the frictional force from the normal force. Use dynamics to get the normal force.

Get the frictional force from the normal force. Use dynamics to get the normal force. . L F n µ k L =00 t µ k = 0.60 = 0 o = 050 lb F n +y +x x = sin y = cos = µf n Is the initial elocity o the car reater than 30 mph? Approach: Use conseration o enery. System: car Initial time: beore you

More information

Equivalent rocking systems: Fundamental rocking parameters

Equivalent rocking systems: Fundamental rocking parameters Equivalent rockin systems: Fundamental rockin parameters M.J. DeJon University of Cambride, United Kindom E.G. Dimitrakopoulos The Hon Kon University of Science and Technoloy SUMMARY Early analytical investiations

More information

Non-Newtonian and Gas-non Newtonian Liquid Flow through Elbows CFD Analysis

Non-Newtonian and Gas-non Newtonian Liquid Flow through Elbows CFD Analysis Journal of Applied Fluid Mechanics, Vol. 6, No. 1, pp. 131-141, 2013. Available online at www.jafmonline.net, ISSN 1735-3572, EISSN 1735-3645. Non-Newtonian and Gas-non Newtonian Liquid Flow throuh Elbows

More information

Conical Pendulum Linearization Analyses

Conical Pendulum Linearization Analyses European J of Physics Education Volume 7 Issue 3 309-70 Dean et al. Conical Pendulum inearization Analyses Kevin Dean Jyothi Mathew Physics Department he Petroleum Institute Abu Dhabi, PO Box 533 United

More information

Journal of Advanced Mechanical Design, Systems, and Manufacturing

Journal of Advanced Mechanical Design, Systems, and Manufacturing Numerical Analysis on Paper Separation Usin the Overlap Separation echanism * Hui CHENG **, Hiroshi IKEDA ** and Kazushi YOSHIDA ** ** echanical Enineerin Research Laboratory, Hitachi Ltd. 8- Horiuchi-machi,

More information

ITB J. Eng. Sci. Vol. 41, No. 1, 2009,

ITB J. Eng. Sci. Vol. 41, No. 1, 2009, ITB J. Eng. Sci. Vol. 41, No. 1, 2009, 65-76 65 ressure Drop Correlation Covering Dilute to Dense Regimes o Solid article-gas Flow in a Vertical Conveying ipe Y. Bindar, N.A. Sutrisniningrum & D. Santiani

More information

5 Shallow water Q-G theory.

5 Shallow water Q-G theory. 5 Shallow water Q-G theory. So far we have discussed the fact that lare scale motions in the extra-tropical atmosphere are close to eostrophic balance i.e. the Rossby number is small. We have examined

More information

IMPLEMENTATION AND ASSESSMENT OF THE INTERFACIAL AREA TRANSPORT EQUATION IN THE SYSTEM ANALYSIS CODE TRACE

IMPLEMENTATION AND ASSESSMENT OF THE INTERFACIAL AREA TRANSPORT EQUATION IN THE SYSTEM ANALYSIS CODE TRACE The Pennsylvania State University The Graduate School College of Engineering IMPLEMENTATION AND ASSESSMENT OF THE INTERFACIAL AREA TRANSPORT EQUATION IN THE SYSTEM ANALYSIS CODE TRACE A Thesis in Nuclear

More information

Review of Numerical Methods for Multiphase Flow

Review of Numerical Methods for Multiphase Flow Title Review o Numerical Methods or Multiphase Flow M. Sommereld Mechanische Verahrenstechnik Zentrum ür Ingenieurwissenschaten 06099 Halle (Saale), Germany www-mvt.iw.uni-halle.de Content o the Lecture

More information

MODELING A METAL HYDRIDE HYDROGEN STORAGE SYSTEM. Apurba Sakti EGEE 520, Mathematical Modeling of EGEE systems Spring 2007

MODELING A METAL HYDRIDE HYDROGEN STORAGE SYSTEM. Apurba Sakti EGEE 520, Mathematical Modeling of EGEE systems Spring 2007 MODELING A METAL HYDRIDE HYDROGEN STORAGE SYSTEM Apurba Sakti EGEE 520, Mathematical Modelin of EGEE systems Sprin 2007 Table of Contents Abstract Introduction Governin Equations Enery balance Momentum

More information

Non-newtonian Rabinowitsch Fluid Effects on the Lubrication Performances of Sine Film Thrust Bearings

Non-newtonian Rabinowitsch Fluid Effects on the Lubrication Performances of Sine Film Thrust Bearings International Journal o Mechanical Engineering and Applications 7; 5(): 6-67 http://www.sciencepublishinggroup.com/j/ijmea doi:.648/j.ijmea.75.4 ISSN: -X (Print); ISSN: -48 (Online) Non-newtonian Rabinowitsch

More information

11 Free vibrations: one degree of freedom

11 Free vibrations: one degree of freedom 11 Free vibrations: one deree of freedom 11.1 A uniform riid disk of radius r and mass m rolls without slippin inside a circular track of radius R, as shown in the fiure. The centroidal moment of inertia

More information

Local Heat Transfer Coefficient Measurements, Using a Transient Imaging Method With an Inverse Scheme

Local Heat Transfer Coefficient Measurements, Using a Transient Imaging Method With an Inverse Scheme Local Heat Transer Coeicient Measurements, Using a Transient Imaging Method With an Inverse Scheme A. EL ABBADI, D. BOUGEARD, B.BAUDOIN Ecole des Mines de Douai, Département Energétique Industrielle, 941,

More information

Fin efficiency of the newly developed Compartmented Coil of a Single Coil Twin Fan System

Fin efficiency of the newly developed Compartmented Coil of a Single Coil Twin Fan System Fin eiciency o the newly developed Compartmented Coil o a Single Coil Twin Fan System ABSTRACT In predicting the perormance o any cooling coil, HVAC designers ace multiold challenges in designing the system

More information

Lecture 25: Heat and The 1st Law of Thermodynamics Prof. WAN, Xin

Lecture 25: Heat and The 1st Law of Thermodynamics Prof. WAN, Xin General Physics I Lecture 5: Heat and he 1st Law o hermodynamics Pro. WAN, Xin xinwan@zju.edu.cn http://zimp.zju.edu.cn/~xinwan/ Latent Heat in Phase Changes Latent Heat he latent heat o vaporization or

More information

ARTICLE IN PRESS. Nuclear Instruments and Methods in Physics Research A

ARTICLE IN PRESS. Nuclear Instruments and Methods in Physics Research A Nuclear Instruments and Methods in Physics Research A 66 (29) 517 522 Contents lists available at ScienceDirect Nuclear Instruments and Methods in Physics Research A journal homepae: www.elsevier.com/locate/nima

More information

39.1 Gradually Varied Unsteady Flow

39.1 Gradually Varied Unsteady Flow 39.1 Gradually Varied Unsteady Flow Gradually varied unsteady low occurs when the low variables such as the low depth and velocity do not change rapidly in time and space. Such lows are very common in

More information

DOI:

DOI: Research Archive Citation or published version: Lijing Zhai, et al, Numerical analysis o the axial heat conduction with variable luid properties in a orced laminar low tube, International Journal o Heat

More information