MODELLING OF VENTILATION AIRFLOW RATES OF SOLAR CHIMNEYS FOR BUILDING INTERGRATION OF RENEWABLE ENERGY DEVICES
|
|
- Frederica Gardner
- 5 years ago
- Views:
Transcription
1 MODELLING OF VENTILATION AIRFLOW RATES OF SOLAR CHIMNEYS FOR BUILDING INTERGRATION OF RENEWABLE ENERGY DEVICES A.G. L, Ph.D., P. Jones, Ph.D., P.G. Zhao, L.P. Wang ABSTRACT Heat transfer process and natural ventlaton effectveness drven by a solar chmney attached to a sdewall of buldng are nvestgated wth CFD technque n detal. In ths paper, condtons and parameters studed n the modellng study are the cavty wdth of the solar chmney, the wall temperature, the heght and breadth of the solar chmney, the rato of outlet area to nlet area as well as the outlet locaton of the solar chmney. The ranges of calculaton parameters focused on a solar chmney wth sngle-sded solar collector (sngle-sded heated wall) cover followng condtons: solar chmney length L =.5m~5.m,breadth B=.1m~.5m,heght H=2.m~ 5.m,and B/H=.5~.25. Heated wall surface temperature Tw s changed n the range of 3 ~7 ; the rato of the outlet area to nlet area A r s changed n the range of.6~.8. It s found that for gven buldng geometry and nlet areas, there s an optmum cavty wdth at whch a maxmum arflow rate can be acheved. Based on the predcton, the arflow rate reaches maxmum when B/H s approxmately 1/1. It s also found that for gven chmney geometry, solar chmney ventlaton flow rate can be ncreased wth the enhancement of chmney heght only the cross sectonal area no more than the crtcal area, because cross secton area has a strong effect on the transtonal and/or turbulent convectve heat transfer n an enclosure. From the vew of economy technology, the optmzed heght of a solar chmney can be determned accordng to the optmzed secton rato of breadth to heght and avalable breadth n practce. It s also noted that optmzed ventlaton flow rate can be obtaned when the outlet area takes the same area as the nlet area. Generally, there s good agreement between the numercal results and avalable expermental data from lterature for a solar chmney. INTRODUCTION In the desgn of new buldngs and retroft of old buldngs, the attenton s turnng towards a more ntegral energy desgn on optmal use of sustanable technologes such as natural ventlaton (daytme comfort ventlaton and nght coolng)(bre/cibse 1997;Brarozz et al. 1999; L et al 2). The current trend s to desgn buldngs responsve to the clmate wth an acceptable ndoor envronment and hgh energy effcency. For example, a recent survey n UK ndcated that 9% of drectors and senor managers preferred natural ventlated buldngs wthout ar-condtonng (Lddament 1997). The lmtatons of conventonal energy sources, n terms of cost and avalablty, and an ncreased awareness of envronment ssues, have led to renewed nterest n passve buldng desgn. One mportant applcaton of ths technology s to ntensfy nteror ventlaton by usng a solar chmney to nduce buoyancy-drven flow. Solar chmney natural ventlaton has hgh ground n both developng and developed countres. For nstance, nnovatve solar chmney natural ventlaton desgn technques have an hstorcal bass and have been advanced n recent years (L 2;Lddament 1997;Gvon 1994; Khedar 2). There are many examples usng chmney effect to ventlaton, coolng and smoke exhaust n Chna: courtyard, Xn Jang arch buldng, and cave dwellngs (L 21). In UK, there has also been a development of solar chmney stack-nduced cross ventlaton desgn for non-domestc buldngs, such as Audtora and Offces, Inland Revenue Headquarters Buldngs located n Nottngham. However, dfferent heated sdes and ar outlet locatons can result n dfferent temperature felds and velocty felds. As a result, the arflow rate and exhaust temperature are also changed. Maor uncertanty n the desgn of solar chmney s the effect of the geometrcal structures, solar radaton and outdoor temperature. Unfortunately, we have lttle knowledge n determnng those parameters for an effcent and effectve desgn of the solar chmney natural Angu L s Professor, School of Envronmental & Muncpal Engneerng, X'an Unversty of Archtecture & Technology, X'an, PR. Chna, Angu L was a Royal Socety KC Wong Fellow from 22 to 23 at Cardff Unversty, U. K.; Phllp Jones s Professor, Head of Welsh School of Archtecture, Cardff Unversty, Cardff, Wales, CF1 3 NB, U. K.; Pngge Zhao and Lpng Wang 1
2 are Graduate students, X'an Unversty of Archtecture & Technology, X'an, PR. Chna. Correspondng author. Tel/Fax.: ; E-mal: ventlaton systems (Pashnamurth 1998;Bansal et al.1993). Ths paper s focused on arflow and convectve heat transfer nsde the solar chmney. The emphass s lad on the comparson between dfferent heated sdes, outlet locatons and the relatonshp between the outlet and nlet area, the temperature dfference, and the optmum structural sze. TURBULENCE MATHEMATIC MODEL AND MITFLOW PROGRAM Ths research s carred out through CFD calculaton wth theoretcal analyses and MITFLOW program, whch was developed by Chen, etc n MIT [1]. The temperature feld and velocty feld are showed by FORTRAN coded program and EXCEL2. About 6 cases have been calculated to fnd out the optmum condton for solar chmney ventlaton desgn. The rate of arflow can be calculated from these equatons n varous szes of solar collector, seeng whether ventlaton requrements can be satsfed. Arflow nsde solar chmney belongs to turbulent flow. In ths research, MITFLOW equaton model based on tme average method s solved. Every grd s n conformty wth the conservaton of mass flow,.e. the nlet mass flow s equal to the outlet flow. For one-sded heated solar chmney turbulent convectve dffuson, ts governng equatons are concluded from the basc equatons n flud dynamcs (contnuty, momentum, energy) and tme average method. When zero governng equaton s concluded, the prmary assumptons are as the followng (1) Arflow nsde solar chmney s low speed, ncompressble and conforms to deal gas law. (2) Indoor ar belongs to Newton fluds whose surface stress s conform to broadly Newton vscosty stress equaton. (3) Boussngq assumpton s appled. Turbulence tme average equatons are obtaned based on the assumptons above. Contnuty Where V average velocty n x coordnate x drecton V X = (1) Momentum Where ρ ar densty ρv ρ VV + t V average velocty n x drecton P pressure µ effectve vscosty coeffcent eff P = + µ β coeffcent of ar thermal expanson T O temperature at the referent pont T ar temperature g acceleraton of gravty n drecton The last rght tem n equaton s buoyancy. V V eff( + ) + ρβ( T T) g (2) Energy In order to determne the temperature dstrbuton and buoyancy tem n (2),energy conservaton equaton should be solved. 2
3 ρt ρvt + t X Where Γ temperature effectve dffusvty T, eff = X q heat source C p specfc heat at constant pressure In ths research, the equaton below s used to estmate the temperature effectve dffusvty. µ eff Γ T, = (4) eff Preff Pr eff general Prandtl number Turbulent effects are unted to turbulent effectve dffusvty, whch s the sum of turbulent dffusvty µ and lamnar vscosty coeffcent. t Γ T, eff µ µ + µ T X + q c p (3) eff = t (5) In the assumpton of Prandtl-Kolmogorov,turbulent dffusvty µ t s the result of turbulent fluctuaton momentum energy and turbulent fluctuaton dmenson.l s used to denote turbulent length proportonal scale. 1/ 2 µ t = C v ρk l (6) Where C v = s emprcal constant (Chen; Glcksman 21). Accordng to the dfferent methods to solve the unknown parameters K and L,the turbulent vscosty models are dvded nto many forms. The smplest model s Prandtl mxng length model. In ths research, turbulent vscosty s denoted wth local average velocty and length scale by the smple algebrac equaton (Chen 21;Afonso et al 2) µ t =. 3874ρVl (7) l length scale, the dstance between envelope and nearest surface. Those equatons can be dscretzed nto algebrac equatons, and a seres of algebrac equatons can be solved by MITFLOW program. Algebrac equatons n up-wnd dfference form are used durng modellng process as used by Chen and Glcksman (21). NUMERICAL SIMULATION RESULTS AND ANALYSES The theoretcal model to descrbe sngle-sded solar chmney s dealzed. Amongst other smplfcatons, t assumes that there s no external wnd; that the densty of the ar outsde the chmney s unform; that the solar collector s derved from a plate of unform temperature; and that the adacent walls of the solar chmney are nsulated. These studes are focused on 4 parameters, that s, H, B/H, A and L. The case geometrcal structures studed for sngle-sded r heated solar chmney are presented n Fg.1. The calculatons on arflow rate m and outlet temperature t out are performed respectvely. The ranges of calculaton parameters are reported below. Solar chmney model sze:l(length) B(breadth) H(heght), L=.5~5.m,B=.1m~.5m,H=2.m~5.m,B/H=.5~.25 Heated wall surface temperature T w = t w +273, t w =3 ~7, t n =2 The rato between outlet area and nlet area A r =.6~.8 In consderng practcal archtecture condtons,the dstance between the upper edge of outlet and the top of solar chmney s.1h. The outlet s located at the heated wall. In ths paper, about 6 cases coverng the nfluence of the solar collector wall temperature t w, nflow temperature t n, solar chmney breadth B, length L, heght H, as well as the rato between 3
4 outlet area and nlet area A r on arflow and outlet (exhaust) temperature t out are smulated n order to understand better the mechansm of solar chmney natural ventlaton. The relatonshp between the arflow rates and solar chmney heght parameter are demonstrated n Fgure Inflow Fgure 1 Vertcal solar chmneys for buldngs. 2 tw=3 Arflow rate (KG/S) Exhaust temperature ( ) H( m) F gur e 2 The r el at on bet ween a r f l ow r at e and ch mney he ght H( m) tw=3 tw=4 tw=5 tw=6 tw=7 tw=4 tw=5 tw=7 F gur e 3 The r el at onsh p bet ween exhaust temperature and chmney he ght 4
5 The arflow rate of solar chmney s notably affected by chmney heght. When the solar collector (wall) temperature s n the range of 3 ~5, arflow rates can reach the maxmum at the heght of H=4m. Meanwhle, from the Fgure 2, when the heght s ncreased to 4 m or more, the ncrease of arflow rate s gradually lower down. Ths phenomena can be partly explaned by the natural convecton n a channel formed by a sngle sothermal plate and an nsulated plate. Only the solar collector surface, whch s an sothermal surface, s nvolved n heat transfer, whle the assocated adacent surfaces beng adabatc. The Nusselt number based on the temperature dfference between the wall and the ambent ar was once proposed by Bar-Cohen (1984). 2 4 c p ρ gβb ( t Nu = 24 µ kh 1 w t ) 1 e (1 ΓH ΓH )(1 e ΓH ) (8) The hghest convectve heat transfer coeffcents can be expected n vertcal channel formed by an sothermal plate and an nsulated plate at a certan heght and wdth (Bar-Cohen, Rohsenow 1984). The arflow rate nsde the solar chmney s exactly produced by the densty dfference or temperature dfference caused by heat transfer. As a consequence, the optmum heght and wdth could be antcpated (see Fgure 6). It s thus possble to select the chmney heght or/and breadth whch wll maxmum the arflows or, alternatvely, choose the heght or breadth whch wll yelds the maxmum heat transfer from the entre solar collector. On the other hand, n fact, the solar chmney to be nvestgated here s three-dmensonal rather than two-dmensonal as a channel mentoned above. The nfluence of three-dmensonal flow,.e., sde nflow, or lateral edge effects, on the arflow should not be gnored. Clearly such effects can be antcpated to become progressvely greater as the surface temperature s ncreased, seeng the curve at the wall temperature t w =7 shown n Fgure 2. The exhaust temperature or outlet temperature s enhanced as the heght or wall temperature s ncreased, as presented n Fgure 3. Arflow rate(kg/s) F gur e 4 The r el at onsh p bet ween a r f l ow r at e and r at o of out l et ar ea t o nl et ar ea From the vew of energy conservatve, the curve tendences are easly to be understood. The exhaust temperature/outlet temperature wll gradually ncrease as the heght or solar collector temperature enhances The relatonshp among arflow rate m, the rato of outlet area to nlet area Ar s shown n Fgure 4. In Fgure 5,the exhaust temperature changes brought about by the rato of outlet exhaust temperature ( C) Ar Ar tw=3 tw=4 tw=5 tw=6 tw=7 F gur e 5 The r el at onsh p bet ween exhaust temper at ur e and r at o of out l et ar ea t o nlet area tw=3 tw=4 tw=5 tw=6 tw=7 5
6 area to nlet area s presented. The exhaust temperature decreases wth the ncrement of outlet areas or decrement of nlet areas. When B/H s vared but parameter condtons L,H,T n,v n and T w reman constant,arflow rate m and outlet temperature t out s predcted and shown n Fgure 6 and Fgure 7. Moreover, arflow rate ncreases wth the heated wall temperature ncreasng. the bgger the rato of outlet area and nlet area, the more the ncreasng value.. 25 In Fgure 6,arflow rate vares wth the varaton of rato of breadth to heght. Arflow rate s up to the maxmum when the rato of breadth to heght s about 1/1.But when the rato s ncreasng further, exceedng 1/1, and arflow rate wll fall down a lot. Ths trend shown n the solar chmney could be explaned by the buoyant plumes characterstcs. Ths mean the reasonable breadth (space) could nduce maxmum ar from the nlet at the bottom. In other words, too much breadth does not create the effectve arflow rate enhancement. Fgure 7 shows that temperature trends at the outlet whle the ratos, breadth to heght, as calculated from MITflow program. When B,L,H,T n,v n and T w reman constant, however, the A r s vared,arflow rate m outlet average temperature t out s nvestgated. The studed cases parameter condtons and outcome are reported n Fgure 8. In fgure 8,arflow rate vares wth the varaton of rato of breadth to heght. Arflow rate s up to the maxmum when the rato of breadth to heght s about.1 ( or 1/1). However, when the rato s ncreasng further to the.15, arflow rate notably fall down a lot. These phenomena also totally concde wth the fact presented n Fgure 6. Agan there s evdence to show that the szes of solar chmney are essental for the heat transfer and the arflow rates. arflow rate(kg/s) exhaust temperature(oc) arflow rate (KG/S) B/ H F gur e 6 The r el at onsh p bet ween a r f l ow r at e and r at o of br eadt h t o he ght tw=3 tw=4 tw=5 tw=6 tw=7 tw=3 tw=4 tw=5 tw=6 tw= B/ H F gur e 7 The r al at onsh p bet ween exhaust temperature and rato of breadth to he ght B/ H=. 5 B/ H=. 1 B/ H=. 15 B/ H=. 2 B/ H=. 25 L(m) F gur e 8 The r el at onsh p bet ween a r f l ow r at e and ch mney he ght 6
7 In Fgure 9, exhaust temperature decreases wth the ncrement of rato of breadth to heght. It mght be the result of ar mxng effect, as the rato of breadth to heght ncreases, there wll be more space (cross sectonal area) for arflow passage gradually. It s also noted that effects on arflows from the breadth change outweghs the effects from heght change. In the range of heght.5 to 5m, the exhaust temperature does not vary much when the heghts enhance but the breadth remans constant. So the sutable solar chmney heght should be selected n desgnng the solar chmney, based on the vew of ventlaton enhancement and economcs. exhaust temperature ( ) L( m) F gur e 9 The r el at onsh p bet ween exhaust temper at ur e and ch mney l engt h B/ H=. 5 B/ H=. 1 B/ H=. 15 B/ H=. 2 B/ H=. 25 The effects of temperature dfference between nlet and outlet on arflow rates are shown n Fgure 1. The bottle neck effect caused by the cross secton appears agan. The arflow rate does not always ncrease wth the enhancement of the temperature dfference between nlet and outlet. The arflow rate wll reach the maxmum at a certan temperature dfference between nlet and outlet for a gven solar chmney szes.. 16 arflow rate(kg/s) T/T n F gur e 1 The r el at onsh p bet ween a r f l ow rate and T/Tn 7
8 CONCLUSIONS By the CFD predcton on the mechansm of natural ventlaton, the relatonshp between the arflow rate and parameters for sngle-sded heated solar chmney s concluded. In the ranges of, solar chmney length L =.5m~5.m,breadth B=.1m~.5m,heght H=2.m~5.m,and B/H =.5~.25, t s found that for a gven buldng geometry and nlet area, there s an optmum cavty wdth at whch a maxmum arflow rate can be acheved. There s a bottle neck effect zone nsde the chmney for the natural ventlaton rates, and natural ventlaton rates are restrcted by ths bottle neck phenomena. Based on the present studed ranges, the arflow rate reaches maxmum when B/H s approxmately 1/1. It s also found that ventlaton mass rate may be ncreased wth the enhancement of chmney heght only the cross sectonal area no more than the crtcal area. From the vew of technology and economy, the optmzed heght of a solar chmney can be determned accordng to the optmzed secton rato of breadth to heght and avalable practcal feld condtons. ACKNOWLEDGEMENTS Ths research proect s sponsored by Royal Socety K C Wong Fellowshp foundaton (U.K.), Chna Natural Scence Foundaton (No ), and SRF for ROCs, SEM. REFERNCES 1 BRE/CIBSE Ventlaton and ar polluton: Buldngs located n urban and cty centres. Buldngs Servces Engneerng Research and Technology. 18 (4), pp Brarozz, G.S., M.S.E.Imbab, E.Noble, and A.C.M.Sousa Physcal and numercal modellng of a solar chmney-based ventlaton system for buldngs. Buldng and Envronment, 27(4),pp L, A.G., and P.J.Jones. 2. Developments n strateges used for natural and mechancal ventlaton n Chna. Indoor + Bult Envronment. 9, pp Lddament, M BRE/CIBSE dscusson and round-up. Buldngs Servces Engneerng Research and Technology. 18 (4), B16-B18 5 L, A.G. and P.J.Jones. 21. Improve passve ventlaton effectveness of buldngs through open-sded ar cowls. IAQVEC. Changsha, Chna 6 Gvon, B Passve and Low Energy Coolng of Buldngs, Van Nostrand Renhold, New York 7 Khedar, J., B.Boonsr, and J.Hrunlabh. 2. Ventlaton mpact of a solar chmney on ndoor temperature fluctuaton and ar change n a school buldng, Energy and Buldngs, 32, pp Pashnamurth N Expermental and theoretcal performance of a demonstraton solar chmney.j. Energy Res., 22, pp Bansal, N.K., R. Mathur, and M.S. Bhandar Solar chmney for enhanced stack ventlaton, Buldng and Envronment, 28 (3), pp Chen Q., and L.R. Glcksman.21. Smplfed methodology to factor room ar movement and the mpact on thermal comfort nto desgn of radatve, convectve and hybrd heatng and coolng systems, ASHRAE RP-927,ASHRAE. 11 Afonso, C. and A. Olvera.2. Solar chmneys: smulaton and experment, Energy and Buldngs, 32 (1), pp Chen, Z.D. and Y. L. 22. Dsplacement natural ventlaton n a sngle-zone buldng wth three level openngs, Buldng and Envronment, 37, pp Bar-Cohen, A. and W.M. Rohsenow Thermally optmum spacng of vertcal, natural convecton cooled, parallel plates, J. Heat Transfer, 16,pp
Heat Transfer and Natural Ventilation Airflow Rates from Single-sided Heated Solar Chimney for Buildings
Heat Transfer and Natural Ventilation Airflow Rates from Single-sided Heated Solar Chimney for Buildings Angui Li* 1, Phillip Jones 2, Pingge Zhao 3 and Liping Wang 3 1 Professor, Department of Environmental
More informationResearch & Reviews: Journal of Engineering and Technology
Research & Revews: Journal of Engneerng and Technology Case Study to Smulate Convectve Flows and Heat Transfer n Arcondtoned Spaces Hussen JA 1 *, Mazlan AW 1 and Hasanen MH 2 1 Department of Mechancal
More informationA NEW FILTERED DYNAMIC SUBGRID-SCALE MODEL FOR LARGE EDDY SIMULATION OF INDOOR AIRFLOW
A NEW FILTERED DYNAMIC SUBGRID-SCALE MODEL FOR LARGE EDDY SIMULATION OF INDOOR AIRFLOW We Zhang and Qngyan Chen Buldng Technology Program Massachusetts Insttute of Technology 77 Mass. Ave., Cambrdge, MA
More informationA Numerical Study of Heat Transfer and Fluid Flow past Single Tube
A Numercal Study of Heat ransfer and Flud Flow past Sngle ube ZEINAB SAYED ABDEL-REHIM Mechancal Engneerng Natonal Research Center El-Bohos Street, Dokk, Gza EGYP abdelrehmz@yahoo.com Abstract: - A numercal
More informationAir Age Equation Parameterized by Ventilation Grouped Time WU Wen-zhong
Appled Mechancs and Materals Submtted: 2014-05-07 ISSN: 1662-7482, Vols. 587-589, pp 449-452 Accepted: 2014-05-10 do:10.4028/www.scentfc.net/amm.587-589.449 Onlne: 2014-07-04 2014 Trans Tech Publcatons,
More informationFORCED CONVECTION HEAT TRANSFER FROM A RECTANGULAR CYLINDER: EFFECT OF ASPECT RATIO
ISTP-,, PRAGUE TH INTERNATIONAL SYMPOSIUM ON TRANSPORT PHENOMENA FORCED CONVECTION HEAT TRANSFER FROM A RECTANGULAR CYLINDER: EFFECT OF ASPECT RATIO Mohammad Rahnama*, Seyed-Mad Hasheman*, Mousa Farhad**
More informationPrinciples of Food and Bioprocess Engineering (FS 231) Solutions to Example Problems on Heat Transfer
Prncples of Food and Boprocess Engneerng (FS 31) Solutons to Example Problems on Heat Transfer 1. We start wth Fourer s law of heat conducton: Q = k A ( T/ x) Rearrangng, we get: Q/A = k ( T/ x) Here,
More informationNumerical Heat and Mass Transfer
Master degree n Mechancal Engneerng Numercal Heat and Mass Transfer 06-Fnte-Dfference Method (One-dmensonal, steady state heat conducton) Fausto Arpno f.arpno@uncas.t Introducton Why we use models and
More informationOperating conditions of a mine fan under conditions of variable resistance
Paper No. 11 ISMS 216 Operatng condtons of a mne fan under condtons of varable resstance Zhang Ynghua a, Chen L a, b, Huang Zhan a, *, Gao Yukun a a State Key Laboratory of Hgh-Effcent Mnng and Safety
More information2 Finite difference basics
Numersche Methoden 1, WS 11/12 B.J.P. Kaus 2 Fnte dfference bascs Consder the one- The bascs of the fnte dfference method are best understood wth an example. dmensonal transent heat conducton equaton T
More informationDUE: WEDS FEB 21ST 2018
HOMEWORK # 1: FINITE DIFFERENCES IN ONE DIMENSION DUE: WEDS FEB 21ST 2018 1. Theory Beam bendng s a classcal engneerng analyss. The tradtonal soluton technque makes smplfyng assumptons such as a constant
More informationBasic concept of reactive flows. Basic concept of reactive flows Combustion Mixing and reaction in high viscous fluid Application of Chaos
Introducton to Toshhsa Ueda School of Scence for Open and Envronmental Systems Keo Unversty, Japan Combuston Mxng and reacton n hgh vscous flud Applcaton of Chaos Keo Unversty 1 Keo Unversty 2 What s reactve
More informationThe Analysis of Convection Experiment
Internatonal Conference on Appled Scence and Engneerng Innovaton (ASEI 5) The Analyss of Convecton Experment Zlong Zhang School of North Chna Electrc Power Unversty, Baodng 7, Chna 469567@qq.com Keywords:
More informationA large scale tsunami run-up simulation and numerical evaluation of fluid force during tsunami by using a particle method
A large scale tsunam run-up smulaton and numercal evaluaton of flud force durng tsunam by usng a partcle method *Mtsuteru Asa 1), Shoch Tanabe 2) and Masaharu Isshk 3) 1), 2) Department of Cvl Engneerng,
More informationREAL TIME AIRFLOW SIMULATION IN BUILDINGS
REAL TIME AIRFLOW SIMULATION IN BUILDINGS Wangda Zuo, and Qngyan (Yan) Chen School of Mechancal Engneerng, Purdue Unversty, West Lafayette, USA ABSTRACT Real tme flow smulaton s crucal n emergency management
More informationOne-sided finite-difference approximations suitable for use with Richardson extrapolation
Journal of Computatonal Physcs 219 (2006) 13 20 Short note One-sded fnte-dfference approxmatons sutable for use wth Rchardson extrapolaton Kumar Rahul, S.N. Bhattacharyya * Department of Mechancal Engneerng,
More informationNUMERICAL SIMULATION ON AIR DISTRIBUTION OF A TENNIS HALL IN WINTER AND EVALUATION ON INDOOR THERMAL ENVIRONMENT
Engneerng Revew, Vol. 34, Issue 2, 109-118, 2014. 109 NUMERICAL SIMULATION ON AIR DISTRIBUTION OF A TENNIS HALL IN WINTER AND EVALUATION ON INDOOR THERMAL ENVIRONMENT X. Su 1* G. Han 2 F. Chen 3 1 School
More informationENERGY SAVING SOLAR FACADE FOR NON-RESIDENTIAL BUILDINGS FOR CLIMATIC CONDITION IN THE CZECH REPUBLIC
ENERGY SAVING SOLAR FACADE FOR NON-RESIDENTIAL BUILDINGS FOR CLIMATIC CONDITION IN THE CZECH REPUBLIC Jr Sedlak and Mlos Kalousek Department of Buldng Desgn Engneerng, Faculty of Cvl Engneerng, Techncal
More informationInfluence of the PCM Layer Location on the Multilayer Wall Thermal Performance
Open Journal of Energy Effcency, 207, 6, -3 http://www.scrp.org/journal/ojee ISSN Onlne: 269-2645 ISSN Prnt: 269-2637 Influence of the PCM Layer Locaton on the Multlayer Wall Thermal Performance Yanna
More informationCHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE
CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE Analytcal soluton s usually not possble when exctaton vares arbtrarly wth tme or f the system s nonlnear. Such problems can be solved by numercal tmesteppng
More informationThe Finite Element Method
The Fnte Element Method GENERAL INTRODUCTION Read: Chapters 1 and 2 CONTENTS Engneerng and analyss Smulaton of a physcal process Examples mathematcal model development Approxmate solutons and methods of
More informationREAL-TIME DETERMINATION OF INDOOR CONTAMINANT SOURCE LOCATION AND STRENGTH, PART II: WITH TWO SENSORS. Beijing , China,
REAL-TIME DETERMIATIO OF IDOOR COTAMIAT SOURCE LOCATIO AD STREGTH, PART II: WITH TWO SESORS Hao Ca,, Xantng L, Wedng Long 3 Department of Buldng Scence, School of Archtecture, Tsnghua Unversty Bejng 84,
More informationSurvey of applications of discrete vortex method in civil engineering
Budownctwo Archtektura 5 (2009) 29-38 Survey of applcatons of dscrete vortex method n cvl engneerng Tomasz Nowck Lubln Unversty of Technology, Faculty of Cvl Engneerng and Archtecture, Department of Structural
More informationUsing Large Eddy Simulation to Study Airflows in and around Buildings
Jang, Y., Su., M., and Chen, Q. 003. Usng large eddy smulaton to study arflows n and around buldngs, ASHRAE Transactons, 109(), 517-56. Usng Large Eddy Smulaton to Study Arflows n and around Buldngs Y
More informationINTERROGATING THE FLOW BEHAVIOUR IN A NOVEL MAGNETIC DESICCANT VENTILATION SYSTEM USING COMPUTATIONAL FLUID DYNAMICS (CFD)
INTERROGATING THE FLOW BEHAVIOUR IN A NOVEL MAGNETIC DESICCANT VENTILATION SYSTEM USING COMPUTATIONAL FLUID DYNAMICS (CFD) Auwal Dodo*, Valente Hernandez-Perez, Je Zhu and Saffa Rffat Faculty of Engneerng,
More informationAn Experimental and Numerical Study on Pressure Drop Coefficient of Ball Valves
A. Ozdomar, K. Turgut Gursel, Y. Pekbey, B. Celkag / Internatonal Energy Journal 8 (2007) An Expermental and Numercal Study on Pressure Drop Coeffcent of Ball Valves www.serd.at.ac.th/rerc A. Ozdamar*
More informationEffect of loading frequency on the settlement of granular layer
Effect of loadng frequency on the settlement of granular layer Akko KONO Ralway Techncal Research Insttute, Japan Takash Matsushma Tsukuba Unversty, Japan ABSTRACT: Cyclc loadng tests were performed both
More informationHEAT TRANSFER IN ELECTRONIC PACKAGE SUBMITTED TO TIME-DEPENDANT CLIMATIC CONDITIONS
ISTP-16, 005, PRAGUE 16 TH INTERNATIONAL SYMPOSIUM ON TRANSPORT PHENOMENA HEAT TRANSFER IN ELECTRONIC PACKAGE SUBMITTED TO TIME-DEPENDANT CLIMATIC CONDITIONS Valére Ménard*, Phlppe Reulet**, Davd Nörtershäuser*,
More informationNumerical Analysis of Natural Ventilation System in a Studio Apartment in Bangladesh
Numercal Analyss of Natural Ventlaton System n a Studo Apartment n Bangladesh K.M Arful Kabr 1, a) Md. Rakbul Hasan 2, b) and Md. Abdul Hakm Khan 1 1 Bangladesh Unversty of Engneerng and Technology, Dhaka-1000,
More informationCalculation of Aerodynamic Characteristics of NACA 2415, 23012, Airfoils Using Computational Fluid Dynamics (CFD)
Calculaton of Aerodynamc Characterstcs of NACA 2415, 23012, 23015 Arfols Usng Computatonal Flud Dynamcs (CFD) Hmanshu Parashar Abstract A method of solvng the flow over arfols of Natonal Advsory Commttee
More informationJ19.1 NUMERICAL SIMULATIONS OF AIRFLOWS AND TRANSPORT AND DIFFUSION FROM WIND TUNNEL TO TERRAIN SCALES
J9. NUMERICAL SIMULATIONS OF AIRFLOWS AND TRANSPORT AND DIFFUSION FROM WIND TUNNEL TO TERRAIN SCALES Tetsuj Yamada Yamada Scence & Art Corporaton, Santa Fe, New Mexco. INTRODUCTION We added CFD (Computatonal
More informationAirflow and Contaminant Simulation with CONTAM
Arflow and Contamnant Smulaton wth CONTAM George Walton, NIST CHAMPS Developers Workshop Syracuse Unversty June 19, 2006 Network Analogy Electrc Ppe, Duct & Ar Wre Ppe, Duct, or Openng Juncton Juncton
More informationThermal-Fluids I. Chapter 18 Transient heat conduction. Dr. Primal Fernando Ph: (850)
hermal-fluds I Chapter 18 ransent heat conducton Dr. Prmal Fernando prmal@eng.fsu.edu Ph: (850) 410-6323 1 ransent heat conducton In general, he temperature of a body vares wth tme as well as poston. In
More informationin a horizontal wellbore in a heavy oil reservoir
498 n a horzontal wellbore n a heavy ol reservor L Mngzhong, Wang Ypng and Wang Weyang Abstract: A novel model for dynamc temperature dstrbuton n heavy ol reservors s derved from and axal dfference equatons
More informationInductance Calculation for Conductors of Arbitrary Shape
CRYO/02/028 Aprl 5, 2002 Inductance Calculaton for Conductors of Arbtrary Shape L. Bottura Dstrbuton: Internal Summary In ths note we descrbe a method for the numercal calculaton of nductances among conductors
More informationNumerical Transient Heat Conduction Experiment
Numercal ransent Heat Conducton Experment OBJECIVE 1. o demonstrate the basc prncples of conducton heat transfer.. o show how the thermal conductvty of a sold can be measured. 3. o demonstrate the use
More informationGravitational Acceleration: A case of constant acceleration (approx. 2 hr.) (6/7/11)
Gravtatonal Acceleraton: A case of constant acceleraton (approx. hr.) (6/7/11) Introducton The gravtatonal force s one of the fundamental forces of nature. Under the nfluence of ths force all objects havng
More informationPostprint.
http://www.dva-portal.org Postprnt Ths s the accepted verson of a paper presented at 13th Internatonal Conference on Indoor Ar Qualty and Clmate, Indoor Ar 214, 7-12 July 214, Hong Kong. Ctaton for the
More information2 MODELS A typcal hgh-sded artculated lorry, whch was nvestgated extensvely by Baker and hs colleagues n wnd tunnels and later used n the dynamc analy
The Seventh Internatonal Colloquum on Bluff Body Aerodynamcs and Applcatons (BBAA7) Shangha, Chna; September 2-6, 2012 Determnaton of aerodynamc characterstcs of a vehcle mmerged n the wake of brdge tower
More informationELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM
ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM An elastc wave s a deformaton of the body that travels throughout the body n all drectons. We can examne the deformaton over a perod of tme by fxng our look
More informationAssessment of Site Amplification Effect from Input Energy Spectra of Strong Ground Motion
Assessment of Ste Amplfcaton Effect from Input Energy Spectra of Strong Ground Moton M.S. Gong & L.L Xe Key Laboratory of Earthquake Engneerng and Engneerng Vbraton,Insttute of Engneerng Mechancs, CEA,
More informationIntroduction to Computational Fluid Dynamics
Introducton to Computatonal Flud Dynamcs M. Zanub 1, T. Mahalakshm 2 1 (PG MATHS), Department of Mathematcs, St. Josephs College of Arts and Scence for Women-Hosur, Peryar Unversty 2 Assstance professor,
More informationIndeterminate pin-jointed frames (trusses)
Indetermnate pn-jonted frames (trusses) Calculaton of member forces usng force method I. Statcal determnacy. The degree of freedom of any truss can be derved as: w= k d a =, where k s the number of all
More informationCOMPARISON OF SOME RELIABILITY CHARACTERISTICS BETWEEN REDUNDANT SYSTEMS REQUIRING SUPPORTING UNITS FOR THEIR OPERATIONS
Avalable onlne at http://sck.org J. Math. Comput. Sc. 3 (3), No., 6-3 ISSN: 97-537 COMPARISON OF SOME RELIABILITY CHARACTERISTICS BETWEEN REDUNDANT SYSTEMS REQUIRING SUPPORTING UNITS FOR THEIR OPERATIONS
More informationESA modelling and cycle design
ESA modellng and cycle desgn WP and WP 5 Unversty of Belgrade MATESA Dssemnaton day, Oslo 16.6.016 Motvaton Develop rgorous 3D models (CFD) to understand the processes, examne the nfluence of condtons
More informationLab 2e Thermal System Response and Effective Heat Transfer Coefficient
58:080 Expermental Engneerng 1 OBJECTIVE Lab 2e Thermal System Response and Effectve Heat Transfer Coeffcent Warnng: though the experment has educatonal objectves (to learn about bolng heat transfer, etc.),
More informationA Mathematical Model for Infiltration Heat Recovery
A Mathematcal Model for Infltraton Heat Recovery C. R. Buchanan and M. H. Sherman 1 Energy Performance of Buldngs Group Indoor Envronment Department Envronmental Energy Technologes Dvson Lawrence Berkeley
More informationSTUDY ON TWO PHASE FLOW IN MICRO CHANNEL BASED ON EXPERI- MENTS AND NUMERICAL EXAMINATIONS
Blucher Mechancal Engneerng Proceedngs May 0, vol., num. www.proceedngs.blucher.com.br/evento/0wccm STUDY ON TWO PHASE FLOW IN MICRO CHANNEL BASED ON EXPERI- MENTS AND NUMERICAL EXAMINATIONS Takahko Kurahash,
More informationχ x B E (c) Figure 2.1.1: (a) a material particle in a body, (b) a place in space, (c) a configuration of the body
Secton.. Moton.. The Materal Body and Moton hyscal materals n the real world are modeled usng an abstract mathematcal entty called a body. Ths body conssts of an nfnte number of materal partcles. Shown
More informationCFD VALIDATION OF STRATIFIED TWO-PHASE FLOWS IN A HORIZONTAL CHANNEL
CFD VALIDATION OF STRATIFIED TWO-PHASE FLOWS IN A HORIZONTAL CHANNEL 1. Introducton Chrstophe Vallée and Thomas Höhne In dfferent scenaros of small break Loss of Coolant Accdent (SB-LOCA), stratfed twophase
More informationComparison of Regression Lines
STATGRAPHICS Rev. 9/13/2013 Comparson of Regresson Lnes Summary... 1 Data Input... 3 Analyss Summary... 4 Plot of Ftted Model... 6 Condtonal Sums of Squares... 6 Analyss Optons... 7 Forecasts... 8 Confdence
More informationNumerical Simulation of Lid-Driven Cavity Flow Using the Lattice Boltzmann Method
Proceedngs of the 3th WSEAS Internatonal Conference on APPLIED MATHEMATICS (MATH'8) Numercal Smulaton of Ld-Drven Cavty Flow Usng the Lattce Boltzmann Method M.A. MUSSA, S. ABDULLAH *, C.S. NOR AZWADI
More informationStatistical Energy Analysis for High Frequency Acoustic Analysis with LS-DYNA
14 th Internatonal Users Conference Sesson: ALE-FSI Statstcal Energy Analyss for Hgh Frequency Acoustc Analyss wth Zhe Cu 1, Yun Huang 1, Mhamed Soul 2, Tayeb Zeguar 3 1 Lvermore Software Technology Corporaton
More informationConstitutive Modelling of Superplastic AA-5083
TECHNISCHE MECHANIK, 3, -5, (01, 1-6 submtted: September 19, 011 Consttutve Modellng of Superplastc AA-5083 G. Gulano In ths study a fast procedure for determnng the constants of superplastc 5083 Al alloy
More informationWeek3, Chapter 4. Position and Displacement. Motion in Two Dimensions. Instantaneous Velocity. Average Velocity
Week3, Chapter 4 Moton n Two Dmensons Lecture Quz A partcle confned to moton along the x axs moves wth constant acceleraton from x =.0 m to x = 8.0 m durng a 1-s tme nterval. The velocty of the partcle
More informationTHE IGNITION PARAMETER - A quantification of the probability of ignition
THE IGNITION PARAMETER - A quantfcaton of the probablty of ton INFUB9-2011 Topc: Modellng of fundamental processes Man author Nels Bjarne K. Rasmussen Dansh Gas Technology Centre (DGC) NBR@dgc.dk Co-author
More informationHigh resolution entropy stable scheme for shallow water equations
Internatonal Symposum on Computers & Informatcs (ISCI 05) Hgh resoluton entropy stable scheme for shallow water equatons Xaohan Cheng,a, Yufeng Ne,b, Department of Appled Mathematcs, Northwestern Polytechncal
More informationElectrical double layer: revisit based on boundary conditions
Electrcal double layer: revst based on boundary condtons Jong U. Km Department of Electrcal and Computer Engneerng, Texas A&M Unversty College Staton, TX 77843-318, USA Abstract The electrcal double layer
More informationSimulated Power of the Discrete Cramér-von Mises Goodness-of-Fit Tests
Smulated of the Cramér-von Mses Goodness-of-Ft Tests Steele, M., Chaselng, J. and 3 Hurst, C. School of Mathematcal and Physcal Scences, James Cook Unversty, Australan School of Envronmental Studes, Grffth
More informationCOMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD
COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD Ákos Jósef Lengyel, István Ecsed Assstant Lecturer, Professor of Mechancs, Insttute of Appled Mechancs, Unversty of Mskolc, Mskolc-Egyetemváros,
More informationLattice Boltzmann simulation of nucleate boiling in micro-pillar structured surface
Proceedngs of the Asan Conference on Thermal Scences 017, 1st ACTS March 6-30, 017, Jeju Island, Korea ACTS-P00545 Lattce Boltzmann smulaton of nucleate bolng n mcro-pllar structured surface Png Zhou,
More informationTurbulent Natural Convection of Heat with Localized Heating and Cooling on Adjacent Vertical Walls in an Enclosure
Internatonal Journal of Scence and esearch (IJS ISSN (Onlne: 319-7064 Turbulent Natural Convecton of Heat wth Localzed Heatng and Coolng on Adacent Vertcal Walls n an Enclosure 1 Chrstopher Onchaga, J.K.Sgey,
More informationFluid structure interaction analysis of a high-pressure regulating valve of a 600-MW ultra-supercritical steam turbine
Orgnal Artcle Flud structure nteracton analyss of a hgh-pressure regulatng valve of a 600-MW ultra-supercrtcal steam turbne Proc IMechE Part A: J Power and Energy 0(0) 1 10! IMechE 2015 Reprnts and permssons:
More informationPsychology 282 Lecture #24 Outline Regression Diagnostics: Outliers
Psychology 282 Lecture #24 Outlne Regresson Dagnostcs: Outlers In an earler lecture we studed the statstcal assumptons underlyng the regresson model, ncludng the followng ponts: Formal statement of assumptons.
More informationLarge Scale Electrostatic Precipitator
11th Internatonal Conference on Electrostatc Precptaton 164 4BStudy and Applcaton of Numercal Calculaton Method for Gas Flow Dstrbuton of Large Scale Electrostatc Precptator DANG Xaoqng, HU Hongsheng,
More informationEXAMPLES of THEORETICAL PROBLEMS in the COURSE MMV031 HEAT TRANSFER, version 2017
EXAMPLES of THEORETICAL PROBLEMS n the COURSE MMV03 HEAT TRANSFER, verson 207 a) What s eant by sotropc ateral? b) What s eant by hoogeneous ateral? 2 Defne the theral dffusvty and gve the unts for the
More informationNumerical Analysis of Heat Transfer and Pressure Drop in a Channel Equipped with Triangular Bodies in Side-By-Side Arrangement
mercal Analyss of Heat Transfer and Pressure Drop n a Channel Equpped wth Trangular Bodes n Sde-By-Sde Arrangement E. Manay Department of Mechancal Engneerng, Faculty of Engneerng, Bayburt Unversty, Bayburt,
More informationTensor Smooth Length for SPH Modelling of High Speed Impact
Tensor Smooth Length for SPH Modellng of Hgh Speed Impact Roman Cherepanov and Alexander Gerasmov Insttute of Appled mathematcs and mechancs, Tomsk State Unversty 634050, Lenna av. 36, Tomsk, Russa RCherepanov82@gmal.com,Ger@npmm.tsu.ru
More informationUncertainty and auto-correlation in. Measurement
Uncertanty and auto-correlaton n arxv:1707.03276v2 [physcs.data-an] 30 Dec 2017 Measurement Markus Schebl Federal Offce of Metrology and Surveyng (BEV), 1160 Venna, Austra E-mal: markus.schebl@bev.gv.at
More informationMing-Chung Chan and Chun-Ho Liu
Large-eddy smulaton of turbulent flows and pollutant transport nsde and above dealzed urban street canyons under dfferent unstable thermal stratfcaton Mng-Chung Chan and Chun-Ho Lu Department of Mechancal
More informationModule 1 : The equation of continuity. Lecture 1: Equation of Continuity
1 Module 1 : The equaton of contnuty Lecture 1: Equaton of Contnuty 2 Advanced Heat and Mass Transfer: Modules 1. THE EQUATION OF CONTINUITY : Lectures 1-6 () () () (v) (v) Overall Mass Balance Momentum
More informationWeek 9 Chapter 10 Section 1-5
Week 9 Chapter 10 Secton 1-5 Rotaton Rgd Object A rgd object s one that s nondeformable The relatve locatons of all partcles makng up the object reman constant All real objects are deformable to some extent,
More informationBack Analysis of Self-Compacting Concrete Rheological Parameters Based on H-B Model
Internatonal Conference on Archtectural, Cvl and Hydraulcs Engneerng (ICACHE 2015) Back Analyss of Self-Compactng Concrete Rheologcal Parameters Based on H-B Model Shua Zeng1, a, Janjun Sh1,b, Wenqang
More informationA Robust Method for Calculating the Correlation Coefficient
A Robust Method for Calculatng the Correlaton Coeffcent E.B. Nven and C. V. Deutsch Relatonshps between prmary and secondary data are frequently quantfed usng the correlaton coeffcent; however, the tradtonal
More information(Online First)A Lattice Boltzmann Scheme for Diffusion Equation in Spherical Coordinate
Internatonal Journal of Mathematcs and Systems Scence (018) Volume 1 do:10.494/jmss.v1.815 (Onlne Frst)A Lattce Boltzmann Scheme for Dffuson Equaton n Sphercal Coordnate Debabrata Datta 1 *, T K Pal 1
More informationNUMERICAL DIFFERENTIATION
NUMERICAL DIFFERENTIATION 1 Introducton Dfferentaton s a method to compute the rate at whch a dependent output y changes wth respect to the change n the ndependent nput x. Ths rate of change s called the
More informationFEATURES OF TURBULENT TRANSPORT OF MOMENTUM AND HEAT IN STABLY STRATIFIED BOUNDARY LAYERS AND THEIR REPRODUCTION IN ATMOSPHERIC MESOSCALE MODELS
C I T E S 009_ Krasnoyarsk 009 FEATURES OF TURBULENT TRANSPORT OF MOMENTUM AND HEAT IN STABLY STRATIFIED BOUNDARY LAYERS AND THEIR REPRODUCTION IN ATMOSPHERIC MESOSCALE MODELS A. F. Kurbatsky Insttute
More informationSimulation and experiment of the effect of clearance of impeller wear-rings on the performance of centrifugal pump
IOP Conference Seres: Earth and Envronmental Scence Smulaton and experment of the effect of clearance of mpeller wear-rngs on the performance of centrfugal pump To cte ths artcle: S X Chen et al 01 IOP
More informationParabola Model with the Application to the Single-Point Mooring System
Journal of Multdscplnary Engneerng Scence and Technology (JMEST) ISSN: 58-93 Vol. Issue 3, March - 7 Parabola Model wth the Applcaton to the Sngle-Pont Moorng System Chunle Sun, Yuheng Rong, Xn Wang, Mengjao
More informationCFD MODELLING OF BUOYANCY-DRIVEN NATURAL VENTILATION OPPOSED BY WIND. LE1 9BH, UK 2 Department of Civil and Environmental Engineering,
Nnth Internatonal IBPSA Conference Montréal, Canada August 15-18, 5 CFD MODELLING OF BUOYANCY-DRIVEN NATURAL VENTILATION OPPOSED BY WIND Malcolm Coo 1, Yngchun J 1 and Gary Hunt 1 Insttute of Energy and
More informationNatural Convection with Localized Heating and Cooling on Opposite Vertical Walls in an Enclosure
The SIJ Transactons on Computer Networks & Communcaton Engneerng (CNCE), Vol. 1, No. 4, September-October 013 Natural Convecton wth Localzed Heatng and Coolng on Opposte Vertcal Walls n an Enclosure Marura
More informationEN40: Dynamics and Vibrations. Homework 4: Work, Energy and Linear Momentum Due Friday March 1 st
EN40: Dynamcs and bratons Homework 4: Work, Energy and Lnear Momentum Due Frday March 1 st School of Engneerng Brown Unversty 1. The fgure (from ths publcaton) shows the energy per unt area requred to
More informationStudy on Effect of Different Porosity on Thermally Driven Heat Transfer in a Centrifugal Force Field
5th Internatonal Conference on Cvl Engneerng and Transportaton (ICCET 015) Study on Effect of Dfferent Porosty on Thermally Drven Heat Transfer n a Centrfugal Force Feld 1 Xa Je1,a*, Chang Ha-png,b, and
More informationGEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE
GEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE Prof. J. N. Mandal Department of cvl engneerng, IIT Bombay, Powa, Mumba 400076, Inda. Tel.022-25767328 emal: cejnm@cvl.tb.ac.n Module - 9 LECTURE - 48
More informationAERODYNAMICS I LECTURE 6 AERODYNAMICS OF A WING FUNDAMENTALS OF THE LIFTING-LINE THEORY
LECTURE 6 AERODYNAMICS OF A WING FUNDAMENTALS OF THE LIFTING-LINE THEORY The Bot-Savart Law The velocty nduced by the sngular vortex lne wth the crculaton can be determned by means of the Bot- Savart formula
More informationTemperature. Chapter Heat Engine
Chapter 3 Temperature In prevous chapters of these notes we ntroduced the Prncple of Maxmum ntropy as a technque for estmatng probablty dstrbutons consstent wth constrants. In Chapter 9 we dscussed the
More informationAPPLICATION OF CFD TOOLS FOR INDOOR AND OUTDOOR ENVIRONMENT DESIGN
, Volume 1, Number 1, p.14-9, 000 APPLICATION OF CFD TOOLS FOR INDOOR AND OUTDOOR ENVIRONMENT DESIGN Q. Chen and J. Srebrc Buldng Technology Program, Department of Archtecture, Massachusetts Insttute of
More informationAnalysis of Unsteady Aerodynamics of a Car Model with Radiator in Dynamic Pitching Motion using LS-DYNA
Analyss of Unsteady Aerodynamcs of a Car Model wth Radator n Dynamc Ptchng Moton usng LS-DYNA Yusuke Nakae 1, Jro Takamtsu 1, Hrosh Tanaka 1, Tsuyosh Yasuk 1 1 Toyota Motor Corporaton 1 Introducton Recently,
More informationInfiltration Heat Recovery in Building Walls: Computational Fluid Dynamics Investigations Results
LBNL-534 Infltraton Heat Recovery n Buldng Walls: Computatonal Flud Dynamcs Investgatons Results Marc O. Abade, Elzabeth U. Fnlayson and Ashok J. Gadgl Lawrence Berkeley Natonal Laboratory Envronmental
More informationDETERMINATION OF TEMPERATURE DISTRIBUTION FOR ANNULAR FINS WITH TEMPERATURE DEPENDENT THERMAL CONDUCTIVITY BY HPM
Ganj, Z. Z., et al.: Determnaton of Temperature Dstrbuton for S111 DETERMINATION OF TEMPERATURE DISTRIBUTION FOR ANNULAR FINS WITH TEMPERATURE DEPENDENT THERMAL CONDUCTIVITY BY HPM by Davood Domr GANJI
More informationUNSTEADY LAMINAR CONVECTION FLOW OVER PERIODIC GROOVES BY USING SIO 2 -WATER NANOFLUID
UNSTEADY LAMINAR CONVECTION FLOW OVER PERIODIC GROOVES BY USING SIO -WATER NANOFLUID AMIRHOSSEIN HESHMATI, MOHAMMAD PARSAZADEH & FARSHID FATHINIA 3,&3 Department of Mechancal Engneerng, Unversty Technology
More informationGlobal Sensitivity. Tuesday 20 th February, 2018
Global Senstvty Tuesday 2 th February, 28 ) Local Senstvty Most senstvty analyses [] are based on local estmates of senstvty, typcally by expandng the response n a Taylor seres about some specfc values
More informationCalculating the Quasi-static Pressures of Confined Explosions Considering Chemical Reactions under the Constant Entropy Assumption
Appled Mechancs and Materals Onlne: 202-04-20 ISS: 662-7482, ol. 64, pp 396-400 do:0.4028/www.scentfc.net/amm.64.396 202 Trans Tech Publcatons, Swtzerland Calculatng the Quas-statc Pressures of Confned
More informationEnergy configuration optimization of submerged propeller in oxidation ditch based on CFD
IOP Conference Seres: Earth and Envronmental Scence Energy confguraton optmzaton of submerged propeller n oxdaton dtch based on CFD To cte ths artcle: S Y Wu et al 01 IOP Conf. Ser.: Earth Envron. Sc.
More informationONE DIMENSIONAL TRIANGULAR FIN EXPERIMENT. Technical Advisor: Dr. D.C. Look, Jr. Version: 11/03/00
ONE IMENSIONAL TRIANGULAR FIN EXPERIMENT Techncal Advsor: r..c. Look, Jr. Verson: /3/ 7. GENERAL OJECTIVES a) To understand a one-dmensonal epermental appromaton. b) To understand the art of epermental
More informationFlow equations To simulate the flow, the Navier-Stokes system that includes continuity and momentum equations is solved
Smulaton of nose generaton and propagaton caused by the turbulent flow around bluff bodes Zamotn Krll e-mal: krart@gmal.com, cq: 958886 Summary Accurate predctons of nose generaton and spread n turbulent
More informationTurbulent Flow. Turbulent Flow
http://www.youtube.com/watch?v=xoll2kedog&feature=related http://br.youtube.com/watch?v=7kkftgx2any http://br.youtube.com/watch?v=vqhxihpvcvu 1. Caothc fluctuatons wth a wde range of frequences and
More informationModal Strain Energy Decomposition Method for Damage Detection of an Offshore Structure Using Modal Testing Information
Thrd Chnese-German Jont Symposum on Coastal and Ocean Engneerng Natonal Cheng Kung Unversty, Tanan November 8-16, 2006 Modal Stran Energy Decomposton Method for Damage Detecton of an Offshore Structure
More informationTurbulence classification of load data by the frequency and severity of wind gusts. Oscar Moñux, DEWI GmbH Kevin Bleibler, DEWI GmbH
Turbulence classfcaton of load data by the frequency and severty of wnd gusts Introducton Oscar Moñux, DEWI GmbH Kevn Blebler, DEWI GmbH Durng the wnd turbne developng process, one of the most mportant
More informationSupplementary Notes for Chapter 9 Mixture Thermodynamics
Supplementary Notes for Chapter 9 Mxture Thermodynamcs Key ponts Nne major topcs of Chapter 9 are revewed below: 1. Notaton and operatonal equatons for mxtures 2. PVTN EOSs for mxtures 3. General effects
More information