Analysis of loop heat pipe performance under varying wick load
|
|
- Daisy Malone
- 5 years ago
- Views:
Transcription
1 - Journal of Mechanical Engineering 51(57-8, UDK - UD Original scientific paper (1.1 Analysis of loop heat pipe performance uner varying wick loa A. Heitor Reis 1,, António F. Miguel 1, an Murat Ayin,3 1 hysics Department, University of Évora, R. Romão Ramalho, 59, Évora, ortugal Évora Geophysics enter, R. Romão Ramalho, 59, Évora, ortugal 3 Dep. of Mech. Engineering, Istanbul echnical University, Gumussuyu, Istanbul, urkey ahr@uevora.pt Abstract Loop heat pipes (LH are heat transfer evices use to enhance cooling of small spaces an basically consist of seale tubes connecting a heat source, the evaporator, whose major part is a porous wick, with a conenser that operates as heat sink. In this paper we analyse the effect of curvature of the liqui vapor interface upon the vapor pressure within wick pores. e show how this effect affects start-up by requiring a ifference between wick an conenser temperatures as higher as wick pore with becomes smaller. e analyse also transient operation an foun that iealy LH are self-ajusting systems that ten to stable operation. e present a formula to escribe the transient regime. he analysis provies also optimization of wick pore with for maximum heat transfer. Optimal pore with is shown to vary with temperature ifference between wick an conenser. It is envisage how this feature may help in LH esign. Introuction Loop heat pipes (LH are heat transfer evices in which a working flui transfers continuously heat from the evaporator to the conenser. LH operate uner a pressure ifference generate at a porous wick (the evaporator an that rives the working flui within the loop (see Fig.1. he pressure ifference is ue to the capillary forces rives the liqui from the conenser into the evaporator while the ifference between the saturation pressures corresponing to the evaporator an conenser temperatures rive the vapor back into the conenser. LH have been broaly use in electronics cooling, spacecraft an other areas. Numerous papers ealing with various aspects of LH performance characteristics have been publishe so far [1-1]. Our purpose is not to review this abunant literature extensively but just to focus on a feature whose complete comprehension remains rather elusive: LH require a pressure ifference across the wick in orer to start properly. his is usually overcome through the use of active evices to assist in the start-up. Although some structural aspects of LH may contribute to start-up problems, we believe that thermoynamics play here the major role. hen analyzing LH cycles it is commonly assume that wick pressure follows lausius-lapeyron equation that relates pressure to temperature at an equilibrium planar liqui-vapor interface. However liqui-vapor interfaces in the wick pores are far from being planar. In fact such interfaces are in a shape of meniscus which implies that the equilibrium vapor pressure follows Kelvin s equation [13,14]: s 4 cos exp LR g where s is the saturation pressure corresponing to a planar interface, is surface tension, is soli/liqui contact angle, is pore with, L is ensity of liqui, R g is the specific gas constant an is temperature. Eq. (1 inicates that liqui can boil in the wick pores even if pressure in the overlying vapor is well bellow the saturation pressure corresponing to a planar interface that is given by lausius-lapeyron equation: (1 h LV s exp 1 1 ( R g where h LV stans for the enthalpy of evaporation an the subscript for reference values. By efining the imensionless temperature = (R g /h LV an imensionless pore iameter 451
2 Nomenclature D uct iameter (m ensity (kg m -3 pore with (m soli/liqui contact angle (ra h LV enthalpy of evaporation (J kg -1 L uct lenght (m Superscript m mass flow rate (kg s -1 non-imensional n number of wick pores pressure (a Subscripts s saturation pressure (a conenser Q heat current ( s -1 eq equilibrium R g specific gas constant (J kg -1 K -1 L liqui temperature (K max maximum value t time (s op optimal wick loa (liqui V vapor surface tension (N m -1 wick kinematic viscosity (m s -1 reference value = ( L h LV /cos, an combining Eqs. (1 an ( we obtain: exp 1 (3 For ifference in temperature such that / <<1, the vapor pressure ifference between two successive menisci an (see Fig. an [13] for etails is: (4 where <> represents the average pressure of the vapor between the menisci. ompensation chamber rimary wick Seconary wick Evaporator Bayonet hen (planar interface Eq. (3 reuces to lausius-lapeyron equation. However, when is finite the vapor pressure is lower than saturation pressure at the same temperature. his effect is as much important as the pore with becomes smaller. As a consequence when both the evaporator an conenser are at the same temperature, vapor pressure in the wick is lower than that in the conenser (see Eq. (4 an [13] for etails: (5 D where D >> are the curvature raiuses of the liquivapor interfaces in the conenser an the wick, respectively. o start LHs one has to surpass this negative pressure ifference by increasing the wick temperature. By using Eq. (4 again, we see that LH start-up can only occur for values of the ratio of wick temperature to conenser temperature higher than: 1 4 (6 his is one of the reasons why LHs require a significant grooves Liqui line line liqui vapor liqui onenser Fig. 1. Schematic representation of a LH (major parts. Fig.. Liqui/vapor interfaces of ifferent curvature raiuses. ressure an temperature of the vapor in equilibrium with the liqui epens upon the raius of curvature of the interface. 45 Reis A.H. - Miguel A.F. - Ayin M. A. H. Reis et al.
3 ifference of wick to conenser temperature in orer to start properly. Otherwise LHs can even start with vapor conensation in the wick, which is recognize as the ability to occasionally start in the reverse irection [1]. Authors of recent LH literature [1-1] o not consier the effect of the curvature of the interface upon the vapor pressure an usually restrict the explanations of start-up ifficulties to features of LH operation. In this paper we aress the problem LH operation uner varying heat loa by taking into account the effect of interface curvature upon pressure of the vapor in the wick. q L Analysis of transient LH operation he sum of the pressure heas an rops along a close path within a LH must be zero. herefore for a LH in a horizontal plane if, V, an L enote the pressure ifferences across the liqui-vapor interface at the wick, between vapor at the conenser an the wick, across the liqui-vapor interface at the conenser an between liqui in the wick an the conenser, respectively (see Fig. 3, this conition reas: + V + + L = (7 he pressure ifference across the liqui-vapor interface in the wick is given by the Young-Laplace equation as [13]: 4cos (8 he vapor pressure ifference between conenser an wick is the sum of the pressure hea given by Eq. (4 with the pressure rop ue to vapor flow (see Fig. 3: V 1 D V D L L (1 LV 3m V V (9 4 4 n DV L V V L L L Fig. 3. Schematic representation of the liqui an vapor phases within the LH as well as pressure ifferences an iameter an length of the liqui an vapor lines. Fig.4 Schematic representation of the liqui vapor interface in the wick. ick loa is represente by that is the wick s pore filling level. In Eq. (9 both imensional an imensionless variables coexist as an intermeiary step towars a final imensionless equation to be presente further on. Also in Eq. (9 m V is vapor flow rate, an are pore with an imensionless pore with, n is the number of wick s pores an the subscripts, V, represent conenser, vapor an wick. e assume planar liqui-vapor interface in the conenser an therefore = (1 By assuming Hagen-oiseuille flow along the liqui line, the pressure rop is given by: L LL L 3m L L ( n DL where m L is liqui flow rate an the subscript L stans for liqui. In the wick, heat ( Q is absorbe almost totally by the liqui phase (see Fig. 4 therefore we assume that Q Q (1 where Q represents the heat current absorbe by the wick at maximum loa (=1. e efine wick s varying loa as: m m Liqui L V (13 n L L By combining Eqs. (7-(13 an aing to the alreay efine an the following imensionless variables: - /( L hlv - t t(q /(n L LhLV Q Q 3 /( L h - L L LV A. H. Reis et al. 3 Analysis of loop heat pipe performance uner varying wick loa 453
4 we arrive at the following equation: L nl L L Q 4 D L L nl n L Q L V (1 L V V L D L L D V (14 In Eq. (14 the first an secon terms represent liqui an vapor pumping heas, respectively while the remaining terms represent pressure rops ue to flui flow. Since D V ;D V an V L Eq. (14 can be simplifie to: H (15 where H 1 (16 Q L is the imensionless total pumping hea. he general solution of Eq. (15 is H A exp( t (17 where A is a constant to be etermine from initial conitions. At t =, H A an when t, the imensionless pumping hea equals equilibrium wick loa, i.e. H eq (18 which implies that for reaching stable (equilibrium operation the total pumping hea H cannot be negative. his equilibrium conition also follows from Eq. (17 with that correspons to liqui flow rate being equal to vapor flow rate. herefore rearranging Eq. (17 one obtains: eq exp( t eq (19 which by taking into account Eq. (1 an the efinitions of Q an t may be also expresse in terms of the heat current absorbe at the wick as Q eq Q Q eq Q Q exp nlh LV t ( Fig. 5. Variation of wick loa with time. Lines correspon to ifferent ratios of start-up loas to equilibrium wick loa. Stable operation may be reache by starting either from above or from bellow equilibrium loa ( that matches stable operation. he variation of wick loa, with time is shown in Fig. 5. e see that stable operation (equilibrium may be (ieally reache either from above or from bellow the equilibrium wick loa. In practice, often the wick is not in equilibrium itself what may lea to aitional troubles in LH operation [1]. However as Fig. 5 shows, LHs have a self-ajusting capacity that enable them to reach stable operation. As H eq >, (see Eq. 18 the total pumping hea has to be always positive in orer LH to start an keep on functioning. From Eq. (16 this implies that start-up must comply with the following inequality: eq.8.4 eq = t tttt 1 /4 (1 / /4 For a planar surface, as the start-up conition woul be > simply. By consiering the efinitions of an we conclue that 3 / is of orer V / L 1 what enables us to consier that the general conition expresse by Eq. (1 is not impeitive of LH functioning. Although Eq. (1 is a necessary conition for LH start-up it oes not represent a sufficient conition. In fact, by Eq. (16 H is the sum of the liqui an the vapor pumping hea. Since the first, 4/, is always positive the secon one may be negative. Nevertheless it is sufficient for LH start-up that wick an conenser temperatures aitionally comply also with Eq. (6. From Eq. (6 we conclue that curvature effects of the wick s liqui-vapor interface become important for = ( L h LV /cos smaller than 1 3 (see Eq. 6. Since ( L h LV /cos 1 1 m -1 significant ifference between wick an conenser temperatures is 454 Reis A.H. - Miguel A.F. - Ayin M. A. H. Reis et al. 4
5 require to start LHs with wick pore withs smaller than.1m. Optimization of wick s pore with for LH esign he analysis of the preceing section may become useful in LH esign as it allows for the optimization of wick pore with. By combining Eqs. (1 an (18 one obtains: 1/ Q eq Q 1 L 4 ( By analyzing Eq. ( we can see that heat absorbe at stable operation Q eq, can be maximize with respect to wick s pore iameter. he optimal pore iameter is a function of wick an conenser temperatures of the form: (3 op which in imensional form reas: op LR g cos Lh LV (4 Eq. (4 shows that wick pore iameter that allows for maximum heat transfer is as smaller as the ifference between wick an conenser temperatures gets higher. On the other en we see that op (planar surface as. In Eq. (4 the term within brackets is of orer 3 V / L 1 while (cos/ L h LV 1-1 m -1. herefore for 1 K an 3K, op is of orer 3m. herefore Eq. (4 may help LH manufacturers in choosing the wick pore iameter that matches optimal performance at prescribe wick an conenser temperatures. onclusions he analysis of loop heat pipe (LH carrie out in this paper shows that curve liqui vapor interfaces may change significantly equilibrium vapor pressure in wick pores of withs of orer 1 m. an smaller. his affects LH start-up by requiring significant ifference between wick an conenser temperatures for start-up to occur. his ifference in temperature gets higher as the wick pore with becomes smaller. Solution of a ifferential equation escribing transient functioning shows that LH are self-ajusting systems that ieally ten to stable operation either if starte from above or from below stable operation points. However LH start-up from below stable operation points are unlikely to occur in LH whose wick pores are of orer 1 m an smaller ue to the above mentione ifference between wick an conenser temperatures require to start-up. Optimization of performance of LH with respect to wick pore with shows that optimal pore with can be relate to wick an conenser temperatures an vary linearly with the arnot coefficient of performance of heat pumps. his aspect may help in choosing the appropriate wick structure for prescribe LH operating conitions. References 1. Ku, J. Operating characteristics of loop heat pipes, roc. 9 th Int. onf. Of Environ. Systems, paper No. 9811, (1999 Denver, USA.. Kamotani, Y,hermocapillary flow uner microgravity Experimental results, Av. Space Res. 4, 1 ( Kaya an. Hoang, Mathematical moeling of loop heat pipes an experimental valiation, J. of hermophysics an Heat ransfer 13, 3, ( I. Muraoka, F. M. Ramos, V. V. Vlassov, Analysis of the operational characteristics an limits of a loop heat pipe with porous element in the conenser, Int. J. of Heat an Mass ransfer 5, 8 ( R. hanratilleke., H. Hatakeyama, an H. Nakagome, Development of cryogenic loop heat pipes, ryogenics 38, ( N. Zhang, Innovative heat pipe systems using a new working flui. Int. omm. Heat Mass ransfer, 8 ( H. F. Smirnov an B. V. Kosoy, Refrigerating heat pipes, Appl. herm. Eng. 1 ( Q. Liao. an. S. Zhao, Evaporative heat transfer in a capillary structure heate by a groove block, J. of hermophysics an Heat ransfer 13, No. 1 ( J. S. Allen, K..Hallinan an J. Lekan, A stuy of the funamental operations of a capillary riven heat transfer evice in both normal an low gravity, AI onference roceeings 4, ( , E. American Institute of hysics, oobury, New York. 1.. Figus, Y. Le Bray, S. Bories, an M. rat Heat an mass transfer with phase change in a porous structure partially heate: continuum moel an pore network simulations, Int. J. of Heat an Mass ransfer 4 ( J. Ku, Operating characteristics of loop heat pipes, Int. onf. on Env. Syst., paper J. Baumann, B. ullimore; J. Ambrose, E. Buchan an B. Yenler, A methoology for enveloping reliable start-up pf LHs. aper nº -85, ( Am. Inst. of Aeronautics an Astronautics, Inc. 13. A. H. Reis, hermoynamics of fluis in mesoporous meia, in D. B. Ingham (E. roc. of NAO Av. St. Inst. on orous Meia, 9- June 3, Oviius Un. ress ( A. H. Reis an R. Rosa, Sorption isotherms as a funamental tool for the analysis of couple heat an mass fluxes in porous meia, J. of orous Meia (to appear in 4. A. H. Reis et al. 5 Analysis of loop heat pipe performance uner varying wick loa 455
Asymptotics of a Small Liquid Drop on a Cone and Plate Rheometer
Asymptotics of a Small Liqui Drop on a Cone an Plate Rheometer Vincent Cregan, Stephen B.G. O Brien, an Sean McKee Abstract A cone an a plate rheometer is a laboratory apparatus use to measure the viscosity
More informationTMA 4195 Matematisk modellering Exam Tuesday December 16, :00 13:00 Problems and solution with additional comments
Problem F U L W D g m 3 2 s 2 0 0 0 0 2 kg 0 0 0 0 0 0 Table : Dimension matrix TMA 495 Matematisk moellering Exam Tuesay December 6, 2008 09:00 3:00 Problems an solution with aitional comments The necessary
More informationAn analytical investigation into filmwise condensation on a horizontal tube in a porous medium with suction at the tube surface
Heat Mass Transfer (29) 45:355 361 DOI 1.17/s231-8-436-y ORIGINAL An analytical investigation into filmwise conensation on a horizontal tube in a porous meium with suction at the tube surface Tong Bou
More informationApplications of First Order Equations
Applications of First Orer Equations Viscous Friction Consier a small mass that has been roppe into a thin vertical tube of viscous flui lie oil. The mass falls, ue to the force of gravity, but falls more
More informationAPPROXIMATE SOLUTION FOR TRANSIENT HEAT TRANSFER IN STATIC TURBULENT HE II. B. Baudouy. CEA/Saclay, DSM/DAPNIA/STCM Gif-sur-Yvette Cedex, France
APPROXIMAE SOLUION FOR RANSIEN HEA RANSFER IN SAIC URBULEN HE II B. Bauouy CEA/Saclay, DSM/DAPNIA/SCM 91191 Gif-sur-Yvette Ceex, France ABSRAC Analytical solution in one imension of the heat iffusion equation
More information(2012) , ISBN
Cregan, V. an O'Brien, Stephen B.G. an McKee, Sean (2012) Asymptotics of a small liqui rop on a cone an plate rheometer. In: Progress in Inustrial Mathematics at ECMI 2010. Mathematics in Inustry: Progress
More informationCritical Size and Particle Growth
Critical Size an article Growth rof. Sotiris E. ratsinis article Technology Laboratory Department of Mechanical an rocess Engineering, ETH Zürich, Switzerlan www.ptl.ethz.ch 1 Nucleation-Conensation A
More informationinflow outflow Part I. Regular tasks for MAE598/494 Task 1
MAE 494/598, Fall 2016 Project #1 (Regular tasks = 20 points) Har copy of report is ue at the start of class on the ue ate. The rules on collaboration will be release separately. Please always follow the
More informationSources and Sinks of Available Potential Energy in a Moist Atmosphere. Olivier Pauluis 1. Courant Institute of Mathematical Sciences
Sources an Sinks of Available Potential Energy in a Moist Atmosphere Olivier Pauluis 1 Courant Institute of Mathematical Sciences New York University Submitte to the Journal of the Atmospheric Sciences
More informationTOWARDS THERMOELASTICITY OF FRACTAL MEDIA
ownloae By: [University of Illinois] At: 21:04 17 August 2007 Journal of Thermal Stresses, 30: 889 896, 2007 Copyright Taylor & Francis Group, LLC ISSN: 0149-5739 print/1521-074x online OI: 10.1080/01495730701495618
More information6. Friction and viscosity in gasses
IR2 6. Friction an viscosity in gasses 6.1 Introuction Similar to fluis, also for laminar flowing gases Newtons s friction law hols true (see experiment IR1). Using Newton s law the viscosity of air uner
More information05 The Continuum Limit and the Wave Equation
Utah State University DigitalCommons@USU Founations of Wave Phenomena Physics, Department of 1-1-2004 05 The Continuum Limit an the Wave Equation Charles G. Torre Department of Physics, Utah State University,
More informationHEAT TRANSFER ENHANCED PARABOLIC TROUGH RECEIVER FOR DSG WITH CAPILLAR SYSTEMS
HEAT TRANSFER ENHANCED PARABOLIC TROUGH RECEIVER FOR DSG WITH CAPILLAR SYSTEMS Rojas, M.E. Parabolic Trough Technology Group, PSA / CIEMAT, Av Complutense,, 8040 Mari, Spain Phone: 34 91 346 6049; Fax:
More informationarxiv: v1 [physics.flu-dyn] 8 May 2014
Energetics of a flui uner the Boussinesq approximation arxiv:1405.1921v1 [physics.flu-yn] 8 May 2014 Kiyoshi Maruyama Department of Earth an Ocean Sciences, National Defense Acaemy, Yokosuka, Kanagawa
More informationTo understand how scrubbers work, we must first define some terms.
SRUBBERS FOR PARTIE OETION Backgroun To unerstan how scrubbers work, we must first efine some terms. Single roplet efficiency, η, is similar to single fiber efficiency. It is the fraction of particles
More informationTHERMODYNAMIC ANALYSIS OF ADSORPTION COOLING CYCLE USING CONSOLIDATED COMPOSITE ADSORBENTS - ETHANOL PAIRS
VOL., NO. 2, OCTOBER 26 ISSN 89-668 26-26 Asian Research Publishing Network (ARPN). All rights reserve. THERMODYNAMIC ANALYSIS OF ADSORPTION COOLING CYCLE USING CONSOLIDATED COMPOSITE ADSORBENTS - ETHANOL
More informationExercise 4 - Hydraulic Systems
Exercise 4 - Hyraulic Systems 4.1 Hyraulic Systems Hyraulic systems are, in general, escribe by the Navier-Stokes equations as you might have learne in flui ynamics courses. In orer to simplify the moeling
More informationState-Space Model for a Multi-Machine System
State-Space Moel for a Multi-Machine System These notes parallel section.4 in the text. We are ealing with classically moele machines (IEEE Type.), constant impeance loas, an a network reuce to its internal
More information3.7 Implicit Differentiation -- A Brief Introduction -- Student Notes
Fin these erivatives of these functions: y.7 Implicit Differentiation -- A Brief Introuction -- Stuent Notes tan y sin tan = sin y e = e = Write the inverses of these functions: y tan y sin How woul we
More informationNUMERICAL STUDY OF THERMAL RADIATIONS AND THERMAL STRATIFICATION MECHANISMS IN MHD CASSON FLUID FLOW. and Sardar Muhammad BILAL c
NUMERICAL STUDY OF THERMAL RADIATIONS AND THERMAL STRATIFICATION MECHANISMS IN MHD CASSON FLUID FLOW Khalil Ur REHMAN b c * Noor Ul SABA b Iffat ZEHRA c Muhamma Yousaf MALIK ab an Sarar Muhamma BILAL c
More informationGeneralization of the persistent random walk to dimensions greater than 1
PHYSICAL REVIEW E VOLUME 58, NUMBER 6 DECEMBER 1998 Generalization of the persistent ranom walk to imensions greater than 1 Marián Boguñá, Josep M. Porrà, an Jaume Masoliver Departament e Física Fonamental,
More informationCalculus of Variations
Calculus of Variations Lagrangian formalism is the main tool of theoretical classical mechanics. Calculus of Variations is a part of Mathematics which Lagrangian formalism is base on. In this section,
More informationDusty Plasma Void Dynamics in Unmoving and Moving Flows
7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Dusty Plasma Voi Dynamics in Unmoving an Moving Flows O.V. Kravchenko*, O.A. Azarova**, an T.A. Lapushkina*** *Scientific an Technological
More informationPAijpam.eu RELATIVE HEAT LOSS REDUCTION FORMULA FOR WINDOWS WITH MULTIPLE PANES Cassandra Reed 1, Jean Michelet Jean-Michel 2
International Journal of Pure an Applie Mathematics Volume 97 No. 4 2014 543-549 ISSN: 1311-8080 (printe version); ISSN: 1314-3395 (on-line version) url: http://www.ijpam.eu oi: http://x.oi.org/10.12732/ijpam.v97i4.13
More informationmodel considered before, but the prey obey logistic growth in the absence of predators. In
5.2. First Orer Systems of Differential Equations. Phase Portraits an Linearity. Section Objective(s): Moifie Preator-Prey Moel. Graphical Representations of Solutions. Phase Portraits. Vector Fiels an
More informationPHYSICAL, CHEMICAL AND BIOLOGICAL ASPECTS OF WATER - Thermal Desalination Processes - Asghar Husain, Adel Al Radif, Ali El-Nashar and Klaus Wagnick
THERMAL DESALINATION PROCESSES Asghar Husain, Ael International Center for Water an Energy Systems, Abu Dhabi, UAE Keywors: Boiling point elevation, Conensation, Evaporation, Flashing, Fouling factor,
More informationTransmission Line Matrix (TLM) network analogues of reversible trapping processes Part B: scaling and consistency
Transmission Line Matrix (TLM network analogues of reversible trapping processes Part B: scaling an consistency Donar e Cogan * ANC Eucation, 308-310.A. De Mel Mawatha, Colombo 3, Sri Lanka * onarecogan@gmail.com
More informationA SIMPLE ENGINEERING MODEL FOR SPRINKLER SPRAY INTERACTION WITH FIRE PRODUCTS
International Journal on Engineering Performance-Base Fire Coes, Volume 4, Number 3, p.95-3, A SIMPLE ENGINEERING MOEL FOR SPRINKLER SPRAY INTERACTION WITH FIRE PROCTS V. Novozhilov School of Mechanical
More information19 Eigenvalues, Eigenvectors, Ordinary Differential Equations, and Control
19 Eigenvalues, Eigenvectors, Orinary Differential Equations, an Control This section introuces eigenvalues an eigenvectors of a matrix, an iscusses the role of the eigenvalues in etermining the behavior
More informationIPA Derivatives for Make-to-Stock Production-Inventory Systems With Backorders Under the (R,r) Policy
IPA Derivatives for Make-to-Stock Prouction-Inventory Systems With Backorers Uner the (Rr) Policy Yihong Fan a Benamin Melame b Yao Zhao c Yorai Wari Abstract This paper aresses Infinitesimal Perturbation
More informationThe influence of the equivalent hydraulic diameter on the pressure drop prediction of annular test section
IOP Conference Series: Materials Science an Engineering PAPER OPEN ACCESS The influence of the equivalent hyraulic iameter on the pressure rop preiction of annular test section To cite this article: A
More informationThe Standard Atmosphere. Dr Andrew French
The Stanar Atmosphere Dr Anrew French 1 The International Stanar Atmosphere (ISA) is an iealize moel of the variation of average air pressure an temperature with altitue. Assumptions: The atmosphere consists
More informationHomework 7 Due 18 November at 6:00 pm
Homework 7 Due 18 November at 6:00 pm 1. Maxwell s Equations Quasi-statics o a An air core, N turn, cylinrical solenoi of length an raius a, carries a current I Io cos t. a. Using Ampere s Law, etermine
More informationChapter 6: Energy-Momentum Tensors
49 Chapter 6: Energy-Momentum Tensors This chapter outlines the general theory of energy an momentum conservation in terms of energy-momentum tensors, then applies these ieas to the case of Bohm's moel.
More informationOptimal Variable-Structure Control Tracking of Spacecraft Maneuvers
Optimal Variable-Structure Control racking of Spacecraft Maneuvers John L. Crassiis 1 Srinivas R. Vaali F. Lanis Markley 3 Introuction In recent years, much effort has been evote to the close-loop esign
More informationLATTICE-BASED D-OPTIMUM DESIGN FOR FOURIER REGRESSION
The Annals of Statistics 1997, Vol. 25, No. 6, 2313 2327 LATTICE-BASED D-OPTIMUM DESIGN FOR FOURIER REGRESSION By Eva Riccomagno, 1 Rainer Schwabe 2 an Henry P. Wynn 1 University of Warwick, Technische
More informationEvaporating droplets tracking by holographic high speed video in turbulent flow
Evaporating roplets tracking by holographic high spee vieo in turbulent flow Loïc Méès 1*, Thibaut Tronchin 1, Nathalie Grosjean 1, Jean-Louis Marié 1 an Corinne Fournier 1: Laboratoire e Mécanique es
More informationModel for Dopant and Impurity Segregation During Vapor Phase Growth
Mat. Res. Soc. Symp. Proc. Vol. 648, P3.11.1-7 2001 Materials Research Society Moel for Dopant an Impurity Segregation During Vapor Phase Growth Craig B. Arnol an Michael J. Aziz Division of Engineering
More informationDiagonalization of Matrices Dr. E. Jacobs
Diagonalization of Matrices Dr. E. Jacobs One of the very interesting lessons in this course is how certain algebraic techniques can be use to solve ifferential equations. The purpose of these notes is
More informationA Simple Model for the Calculation of Plasma Impedance in Atmospheric Radio Frequency Discharges
Plasma Science an Technology, Vol.16, No.1, Oct. 214 A Simple Moel for the Calculation of Plasma Impeance in Atmospheric Raio Frequency Discharges GE Lei ( ) an ZHANG Yuantao ( ) Shanong Provincial Key
More informationEfficient Macro-Micro Scale Coupled Modeling of Batteries
A00 Journal of The Electrochemical Society, 15 10 A00-A008 005 0013-651/005/1510/A00/7/$7.00 The Electrochemical Society, Inc. Efficient Macro-Micro Scale Couple Moeling of Batteries Venkat. Subramanian,*,z
More information1. Filling an initially porous tube under a constant head imposed at x =0
Notes on Moving Bounary problems, Voller U o M, volle00@umn.eu. Filling an initially porous tube uner a constant hea impose at x =0 Governing equation is base on calculating the water volume lux by the
More informationOn Characterizing the Delay-Performance of Wireless Scheduling Algorithms
On Characterizing the Delay-Performance of Wireless Scheuling Algorithms Xiaojun Lin Center for Wireless Systems an Applications School of Electrical an Computer Engineering, Purue University West Lafayette,
More informationA new proof of the sharpness of the phase transition for Bernoulli percolation on Z d
A new proof of the sharpness of the phase transition for Bernoulli percolation on Z Hugo Duminil-Copin an Vincent Tassion October 8, 205 Abstract We provie a new proof of the sharpness of the phase transition
More informationSelf-validated calculation of characteristics of a Francis turbine and the mechanism of the S-shape operational instability
IOP Conference Series: Earth an Environmental Science Self-valiate calculation of characteristics of a Francis turbine an the mechanism of the S-shape operational instability To cite this article: Z Zhang
More informationConvective heat transfer
CHAPTER VIII Convective heat transfer The previous two chapters on issipative fluis were evote to flows ominate either by viscous effects (Chap. VI) or by convective motion (Chap. VII). In either case,
More informationInfluence of Radiation on Product Yields in a Film Boiling Reactor
R&D NOTES Influence of Raiation on Prouct Yiels in a Film Boiling Reactor C. Thomas Aveisian, Wing Tsang, Terence Daviovits, an Jonah R. Allaben Sibley School of Mechanical an Aerospace Engineering, Cornell
More informationSection 2.7 Derivatives of powers of functions
Section 2.7 Derivatives of powers of functions (3/19/08) Overview: In this section we iscuss the Chain Rule formula for the erivatives of composite functions that are forme by taking powers of other functions.
More informationELEC3114 Control Systems 1
ELEC34 Control Systems Linear Systems - Moelling - Some Issues Session 2, 2007 Introuction Linear systems may be represente in a number of ifferent ways. Figure shows the relationship between various representations.
More informationParametrization of non-convective condensation processes May 1987
Parametrization of non-convective conensation processes May 987 By M. Tietke European Centre for Meium-Range Weather Forecasts Table of contents. Thermoynamics of moist air 2. Clou physical processes 2.
More informationChapter 11: Feedback and PID Control Theory
Chapter 11: Feeback an D Control Theory Chapter 11: Feeback an D Control Theory. ntrouction Feeback is a mechanism for regulating a physical system so that it maintains a certain state. Feeback works by
More information'HVLJQ &RQVLGHUDWLRQ LQ 0DWHULDO 6HOHFWLRQ 'HVLJQ 6HQVLWLYLW\,1752'8&7,21
Large amping in a structural material may be either esirable or unesirable, epening on the engineering application at han. For example, amping is a esirable property to the esigner concerne with limiting
More informationOne Dimensional Convection: Interpolation Models for CFD
One Dimensional Convection: Interpolation Moels for CFD ME 448/548 Notes Geral Recktenwal Portlan State University Department of Mechanical Engineering gerry@p.eu ME 448/548: D Convection-Di usion Equation
More informationPhysics 2212 K Quiz #2 Solutions Summer 2016
Physics 1 K Quiz # Solutions Summer 016 I. (18 points) A positron has the same mass as an electron, but has opposite charge. Consier a positron an an electron at rest, separate by a istance = 1.0 nm. What
More informationSensors & Transducers 2015 by IFSA Publishing, S. L.
Sensors & Transucers, Vol. 184, Issue 1, January 15, pp. 53-59 Sensors & Transucers 15 by IFSA Publishing, S. L. http://www.sensorsportal.com Non-invasive an Locally Resolve Measurement of Soun Velocity
More informationθ x = f ( x,t) could be written as
9. Higher orer PDEs as systems of first-orer PDEs. Hyperbolic systems. For PDEs, as for ODEs, we may reuce the orer by efining new epenent variables. For example, in the case of the wave equation, (1)
More informationThermodynamic basis for a variational model for crystal growth
PHYSICL REIEW E OLUME 60, NUMBER 1 JULY 1999 Thermoynamic basis for a variational moel for crystal growth Bayar K. Johnson* an Robert F. Sekerka Carnegie Mellon University, Pittsburgh, Pennsylvania 1513
More informationensembles When working with density operators, we can use this connection to define a generalized Bloch vector: v x Tr x, v y Tr y
Ph195a lecture notes, 1/3/01 Density operators for spin- 1 ensembles So far in our iscussion of spin- 1 systems, we have restricte our attention to the case of pure states an Hamiltonian evolution. Toay
More informationwater adding dye partial mixing homogenization time
iffusion iffusion is a process of mass transport that involves the movement of one atomic species into another. It occurs by ranom atomic jumps from one position to another an takes place in the gaseous,
More informationSchrödinger s equation.
Physics 342 Lecture 5 Schröinger s Equation Lecture 5 Physics 342 Quantum Mechanics I Wenesay, February 3r, 2010 Toay we iscuss Schröinger s equation an show that it supports the basic interpretation of
More informationSimulation of Angle Beam Ultrasonic Testing with a Personal Computer
Key Engineering Materials Online: 4-8-5 I: 66-9795, Vols. 7-73, pp 38-33 oi:.48/www.scientific.net/kem.7-73.38 4 rans ech ublications, witzerlan Citation & Copyright (to be inserte by the publisher imulation
More informationConservation laws a simple application to the telegraph equation
J Comput Electron 2008 7: 47 51 DOI 10.1007/s10825-008-0250-2 Conservation laws a simple application to the telegraph equation Uwe Norbrock Reinhol Kienzler Publishe online: 1 May 2008 Springer Scienceusiness
More informationA simple model for the small-strain behaviour of soils
A simple moel for the small-strain behaviour of soils José Jorge Naer Department of Structural an Geotechnical ngineering, Polytechnic School, University of São Paulo 05508-900, São Paulo, Brazil, e-mail:
More informationPredictive Control of a Laboratory Time Delay Process Experiment
Print ISSN:3 6; Online ISSN: 367-5357 DOI:0478/itc-03-0005 Preictive Control of a aboratory ime Delay Process Experiment S Enev Key Wors: Moel preictive control; time elay process; experimental results
More informationLecture XII. where Φ is called the potential function. Let us introduce spherical coordinates defined through the relations
Lecture XII Abstract We introuce the Laplace equation in spherical coorinates an apply the metho of separation of variables to solve it. This will generate three linear orinary secon orer ifferential equations:
More informationOn the number of isolated eigenvalues of a pair of particles in a quantum wire
On the number of isolate eigenvalues of a pair of particles in a quantum wire arxiv:1812.11804v1 [math-ph] 31 Dec 2018 Joachim Kerner 1 Department of Mathematics an Computer Science FernUniversität in
More informationThermal conductivity of graded composites: Numerical simulations and an effective medium approximation
JOURNAL OF MATERIALS SCIENCE 34 (999)5497 5503 Thermal conuctivity of grae composites: Numerical simulations an an effective meium approximation P. M. HUI Department of Physics, The Chinese University
More informationControl of a PEM Fuel Cell Based on a Distributed Model
21 American Control Conference Marriott Waterfront, Baltimore, MD, USA June 3-July 2, 21 FrC1.6 Control of a PEM Fuel Cell Base on a Distribute Moel Michael Mangol Abstract To perform loa changes in proton
More informationON THE OPTIMALITY SYSTEM FOR A 1 D EULER FLOW PROBLEM
ON THE OPTIMALITY SYSTEM FOR A D EULER FLOW PROBLEM Eugene M. Cliff Matthias Heinkenschloss y Ajit R. Shenoy z Interisciplinary Center for Applie Mathematics Virginia Tech Blacksburg, Virginia 46 Abstract
More informationChapter 11: Feedback and PID Control Theory
Chapter 11: Feeback an D Control Theory Chapter 11: Feeback an D Control Theory. ntrouction Feeback is a mechanism for regulating a physical system so that it maintains a certain state. Feeback works by
More informationSparse Reconstruction of Systems of Ordinary Differential Equations
Sparse Reconstruction of Systems of Orinary Differential Equations Manuel Mai a, Mark D. Shattuck b,c, Corey S. O Hern c,a,,e, a Department of Physics, Yale University, New Haven, Connecticut 06520, USA
More information739. Design of adaptive sliding mode control for spherical robot based on MR fluid actuator
739. Design of aaptive sliing moe control for spherical robot base on MR flui actuator M. Yue,, B. Y. Liu School of Automotive Engineering, Dalian University of echnology 604, Dalian, Liaoning province,
More informationEvaluation of Column Breakpoint and Trajectory for a Plain Liquid Jet Injected into a Crossflow
ILASS Americas, 1 st Annual Conference on Liqui Atomization an Spray Systems, Orlano, Floria, May 008 Evaluation of Column Breakpoint an Trajectory for a Plain Liqui Jet Injecte into a Crossflow S.M. Thawley,
More informationLinear analysis of a natural circulation driven supercritical water loop
TU Delft Bachelor Thesis Linear analysis of a natural circulation riven supercritical water loop D J van er Ham 4285816 supervise by Dr. Ir. M. Rohe July 3, 216 Nomenclature Symbol Units Description A
More informationNOTES ON EULER-BOOLE SUMMATION (1) f (l 1) (n) f (l 1) (m) + ( 1)k 1 k! B k (y) f (k) (y) dy,
NOTES ON EULER-BOOLE SUMMATION JONATHAN M BORWEIN, NEIL J CALKIN, AND DANTE MANNA Abstract We stuy a connection between Euler-MacLaurin Summation an Boole Summation suggeste in an AMM note from 196, which
More informationTutorial Test 5 2D welding robot
Tutorial Test 5 D weling robot Phys 70: Planar rigi boy ynamics The problem statement is appene at the en of the reference solution. June 19, 015 Begin: 10:00 am En: 11:30 am Duration: 90 min Solution.
More informationChapter 4. Electrostatics of Macroscopic Media
Chapter 4. Electrostatics of Macroscopic Meia 4.1 Multipole Expansion Approximate potentials at large istances 3 x' x' (x') x x' x x Fig 4.1 We consier the potential in the far-fiel region (see Fig. 4.1
More informationarxiv: v1 [cond-mat.stat-mech] 9 Jan 2012
arxiv:1201.1836v1 [con-mat.stat-mech] 9 Jan 2012 Externally riven one-imensional Ising moel Amir Aghamohammai a 1, Cina Aghamohammai b 2, & Mohamma Khorrami a 3 a Department of Physics, Alzahra University,
More informationA note on the Mooney-Rivlin material model
A note on the Mooney-Rivlin material moel I-Shih Liu Instituto e Matemática Universiae Feeral o Rio e Janeiro 2945-97, Rio e Janeiro, Brasil Abstract In finite elasticity, the Mooney-Rivlin material moel
More informationTable of Common Derivatives By David Abraham
Prouct an Quotient Rules: Table of Common Derivatives By Davi Abraham [ f ( g( ] = [ f ( ] g( + f ( [ g( ] f ( = g( [ f ( ] g( g( f ( [ g( ] Trigonometric Functions: sin( = cos( cos( = sin( tan( = sec
More informationMath 1271 Solutions for Fall 2005 Final Exam
Math 7 Solutions for Fall 5 Final Eam ) Since the equation + y = e y cannot be rearrange algebraically in orer to write y as an eplicit function of, we must instea ifferentiate this relation implicitly
More informationQubit channels that achieve capacity with two states
Qubit channels that achieve capacity with two states Dominic W. Berry Department of Physics, The University of Queenslan, Brisbane, Queenslan 4072, Australia Receive 22 December 2004; publishe 22 March
More informationStrength Analysis of CFRP Composite Material Considering Multiple Fracture Modes
5--XXXX Strength Analysis of CFRP Composite Material Consiering Multiple Fracture Moes Author, co-author (Do NOT enter this information. It will be pulle from participant tab in MyTechZone) Affiliation
More informationSIMULATION OF DIRECT CONTACT CONDENSATION OF STEAM JETS SUBMERGED IN SUBCOOLED WATER BY MEANS OF A ONE-DIMENSIONAL TWO-FLUID MODEL
HEFAT014 10 th International Conference on Heat Transfer, Flui Mechanics an Thermoynamics 14 16 July 014 Orlano, Floria SIMULATION OF DIRECT CONTACT CONDENSATION OF STEAM JETS SUBMERGED IN SUBCOOLED WATER
More informationSeparation of Variables
Physics 342 Lecture 1 Separation of Variables Lecture 1 Physics 342 Quantum Mechanics I Monay, January 25th, 2010 There are three basic mathematical tools we nee, an then we can begin working on the physical
More informationSystems & Control Letters
Systems & ontrol Letters ( ) ontents lists available at ScienceDirect Systems & ontrol Letters journal homepage: www.elsevier.com/locate/sysconle A converse to the eterministic separation principle Jochen
More informationClosed and Open Loop Optimal Control of Buffer and Energy of a Wireless Device
Close an Open Loop Optimal Control of Buffer an Energy of a Wireless Device V. S. Borkar School of Technology an Computer Science TIFR, umbai, Inia. borkar@tifr.res.in A. A. Kherani B. J. Prabhu INRIA
More informationOn Using Unstable Electrohydraulic Valves for Control
Kailash Krishnaswamy Perry Y. Li Department of Mechanical Engineering, University of Minnesota, 111 Church St. SE, Minneapolis, MN 55455 e-mail: kk,pli @me.umn.eu On Using Unstable Electrohyraulic Valves
More informationThis section outlines the methodology used to calculate the wave load and wave wind load values.
COMPUTERS AND STRUCTURES, INC., JUNE 2014 AUTOMATIC WAVE LOADS TECHNICAL NOTE CALCULATION O WAVE LOAD VALUES This section outlines the methoology use to calculate the wave loa an wave win loa values. Overview
More information1 dx. where is a large constant, i.e., 1, (7.6) and Px is of the order of unity. Indeed, if px is given by (7.5), the inequality (7.
Lectures Nine an Ten The WKB Approximation The WKB metho is a powerful tool to obtain solutions for many physical problems It is generally applicable to problems of wave propagation in which the frequency
More informationChapter 2 Governing Equations
Chapter 2 Governing Equations In the present an the subsequent chapters, we shall, either irectly or inirectly, be concerne with the bounary-layer flow of an incompressible viscous flui without any involvement
More informationAn Application of Homotopy Analysis Method for Estimation the Diaphragm Deflection in MEMS Capacitive Microphone
ISSN 1749-3889 (print, 1749-3897 (online International Journal of Nonlinear Science Vol.17(2014 No.1,pp.3-13 An Application of Homotopy Analysis Metho for Estimation the Diaphragm Deflection in MEMS Capacitive
More informationarxiv:physics/ v2 [physics.ed-ph] 23 Sep 2003
Mass reistribution in variable mass systems Célia A. e Sousa an Vítor H. Rorigues Departamento e Física a Universiae e Coimbra, P-3004-516 Coimbra, Portugal arxiv:physics/0211075v2 [physics.e-ph] 23 Sep
More informationChapter-2. Steady Stokes flow around deformed sphere. class of oblate axi-symmetric bodies
hapter- Steay Stoes flow aroun eforme sphere. class of oblate axi-symmetric boies. General In physical an biological sciences, an in engineering, there is a wie range of problems of interest lie seimentation
More informationExperimental Robustness Study of a Second-Order Sliding Mode Controller
Experimental Robustness Stuy of a Secon-Orer Sliing Moe Controller Anré Blom, Bram e Jager Einhoven University of Technology Department of Mechanical Engineering P.O. Box 513, 5600 MB Einhoven, The Netherlans
More informationDynamic Load Carrying Capacity of Spatial Cable Suspended Robot: Sliding Mode Control Approach
Int J Avance Design an Manufacturing echnology, Vol. 5/ No. 3/ June - 212 73 Dynamic Loa Carrying Capacity of Spatial Cable Suspene Robot: Sliing Moe Control Approach M. H. Korayem Department of Mechanical
More informationThe derivative of a function f(x) is another function, defined in terms of a limiting expression: f(x + δx) f(x)
Y. D. Chong (2016) MH2801: Complex Methos for the Sciences 1. Derivatives The erivative of a function f(x) is another function, efine in terms of a limiting expression: f (x) f (x) lim x δx 0 f(x + δx)
More informationA Short Note on Self-Similar Solution to Unconfined Flow in an Aquifer with Accretion
Open Journal o Flui Dynamics, 5, 5, 5-57 Publishe Online March 5 in SciRes. http://www.scirp.org/journal/oj http://x.oi.org/.46/oj.5.57 A Short Note on Sel-Similar Solution to Unconine Flow in an Aquier
More information3-D FEM Modeling of fiber/matrix interface debonding in UD composites including surface effects
IOP Conference Series: Materials Science an Engineering 3-D FEM Moeling of fiber/matrix interface eboning in UD composites incluing surface effects To cite this article: A Pupurs an J Varna 2012 IOP Conf.
More informationPolynomial Inclusion Functions
Polynomial Inclusion Functions E. e Weert, E. van Kampen, Q. P. Chu, an J. A. Muler Delft University of Technology, Faculty of Aerospace Engineering, Control an Simulation Division E.eWeert@TUDelft.nl
More information