Turbulent entry length. 7.3 Turbulent pipe flow. Turbulent entry length. Illustrative experiment. The Reynolds analogy and heat transfer
|
|
- Brenda Brown
- 6 years ago
- Views:
Transcription
1 Turulet etry legt 7.3 Turulet ie l Etry legts x e ad x et are geerally srter turulet l ta lamar l Termal etry legts, x et /, r a case it q cst imsed a ydrdyamically ully develed l 7.3 Turulet ie l ill e mre ta 5% e its ully develed value turulet l Fr liquid metal x et is very lg ad strgly deed Re ad Pr Fr gases ad metallic liquid, x et is t strgly sesitive t Re, Fr metallic liquid, Pr>, δ t < δ, δ t is very t, x et a e Turulet etry legt Sae te let ad uirm l ill legte x et Batti ad Sa crrelati (L/>3, Pr 0.7 C + ( L / 7.3 Turulet ie l ully develed value te sselt umer Cstats r te gas-l simultaeus etry legt crrelati, r varius let ciguratis. Illustrative exerimet Kreit exerimetal data (Re, Pr, x/ (Re, Pr Te data als relect etry legt Lamar l 3.66 at Re 750 ~ 0 Trasiti rage, greatly, at Re 0 ~ Turulet ie l T cst Turulet regi Re, r R e > 5000 Heat traser t air l a l I.., 60. lg ie 3 4 Recall: lat surace turulet udary layer C ( x/ St x Pr ρcu +.8[Pr ] C ( x / Fr ully develed ie l q u u C ( x C cst T T Nt valid at very l Pr Valid eiter q cst r T cst Valid ly t smt all 7.3 Turulet ie l 7.3 Turulet ie l arcy-weisac ricti actr ead lss Δ ie legt ρu L ρu Wall stress ricti rce luid Δ[( π / 4 ] Δ surace area ie π L 4L S Δ Δ 4C C L ρu ρu ρu ρu / 4L 4 4 Fr ully develed l ( /8Re Pr [Pr ] / 8 5 6
2 Pie ricti actrs 7.3 Turulet ie l ε ( Δδ Histrical rmulatis C /3 /3 /3 St Pr Pr r Re Pr ( / 8 8 Fr smt ie( 4 < Re < /3 C 0.03Re Pr 0. 4 Re Prerties are evaluated at mea T mea (T +T / 7.3 Turulet ie l We (T T is large eug t cause serius cage μ μ /3 0.03Re Pr μ 0.4 Fr liquid Maximum errr +5% ~ -40% 0.67 Pr Mder rmulatis Fully develed l smt ie, Petuv (950 eq. ( /8Re Pr / [Pr ] / 8 Caracteristic Temerature T ricti actr (.8lg Re.64 Trasiti l, Gielsi /3.7[Pr ] /8 7.3 Turulet ie l 4 6 < Re < < Pr < 00 r 6% accuracy 00 Pr < 000 r % accuracy ( / 8(Re 00 Pr Re 5 + Rug-alled ies Rugess a ie all disrut te viscus ad termal sulayer Tyical all rugess cmmercial ies e e Recall: ticess te sulayer δsulayer 30 ere u ricti velcity u ρ ee: rugess Reylds umer Re ε u ε /8 Reε Re Re u u ε ε ρu ε u u ρ Turulet ie l 9 Variatis ysical rerties Variati is accuted y viscsity rati r temerature rati Fr liquid (e 0.5 μ /μ.5 μ 0. r T > T ere μ 0.5 r T < T (7 μ / μ / 6 r T > T K ere K T 0.4 ( μ / μ r T < T Fr gases (e 0.7 T /T Turulet ie l T 0.47 r T > T ere T 0.36 r T < T m T 0.5 r T > T ere m T 0.38 r T < T Hydraulically smt Re ε < 5 Trasitial rug 5 Re ε 70 Fully rug 70 < Re ε Fr ully rug regime, Batti ad Sa 4 ( /8Re Pr Re (4.5Reε Pr 8.48 / Pr Were 0.00 ε / ε /.8lg + Re 3.7 At te same Re, rug > smt, rug > smt 7.3 Turulet ie l
3 7.3 Turulet ie l Heat traser t ully develed ls tues Velcity ad temerature riles durg ully develed turulet l a ie. We Pr <<, liquid metal, δ <δ t, T is t lueced y sulayer, vais rm uctial equati (Pe Pr α We Pr >>, il, δ > δ t, T is lueced y sulayer, is very imrtat ully develed liquid-metal ls tues liquid metals eated lg tues it q cst q Fr T cst: Fr q cst: Pe Pe 7.3 Turulet ie l raly ( Te metal did t et te er surace ( Imurities te metal Treerece ( T + Tut / L/ > 60 Pe u/ α > Heat traser surace vieed Ojectives A ie it T cst, 7.4 Heat traser surace vieed is, t d Q A( T T??? 7.4 Heat traser surace vieed as a eat excager Suc a secti ie ca e vieed it verall eat traser ceiciet U Q ( mc ( T T A( LMT ut Were ( T T ( ut T T LMT T T ut l T T T dx T T ut 5 6 Heat traser surace vieed I T, T ut, T, ad is, t d A mc( T T ut A ( ( LMT I T, T, ad is, t d T ut, Q qpdx P( T T dx mc dt By tegrati 0 L P T ut dt ( T dx Were mc T ( T T 7.4 Heat traser surace vieed L dx L 0 PL T T T T ut ut PL l ex mc T T T T mc Valid t lamar ad turulet ls ducts ay crss secti H t d T ut i q cst??? Examle 7.5 Fully termally develed air l T 0 C, cm, u 0.7m/s, T 60 C T d T x0.5? sluti u Re 4 Lamar l W/m T T ut PL π L ex ex T T mc /4 ρuc π T 0.698( T -T + T 47.9 C ut 7.4 Heat traser surace vieed 7 8
4 Hydraulic diameter Hydraulic diameter 4A c Factr 4 t esure r circular duct P r circular ducts i a 4a a a+ a+ π πi 4( 4 4 π ( + i i e a >> 9 0 Turulet l circular ducts All qualitative ideas develed r circular ducts still valid r circular duct Use lace t calculate ad T turulet l it te rmula circular duct lace t calculate ad m ad u must e ased true crss secti area Examle 7.6 Air l square duct, T 7 C, u m/s, utside te duct T 37 C, utside 5W/m K T d T ut Sluti 4a a a+ 5m u Re 90 > 300 Turulet l T evaluate T ut T T 4 ut U L ex T T ρu c Examle 7.6 T d y eq.(7.43 ad eq. (7.4 ( / 8(Re 00 Pr + /3.7[Pr ] / W/m U +.33W/m side utside T T 4 ut U L ex T T ρu c (.8lg Re.64 Lamar l circular ducts Fl etee arallel late u 3 y 4 u Lamar, ully develed sselt umers ased ydraulic diameters T ut 3.3 C errr 0% ~ % 3 4
5 7.6 Heat traser durg crss l ver cylders Hmer
Chapter 8 Internal Forced Convection
Chater 8 Internal Forced Convection 8.1 Hydrodynamic Considerations 8.1.1 Flow Conditions may be determined exerimentally, as shown in Figs. 7.1-7.2. Re D ρumd μ where u m is the mean fluid velocity over
More informationMotor Stability. Plateau and Mesa Burning
Mtr Stability Recall mass cservati fr steady erati ( =cstat) m eit m b b r b s r m icr m eit Is this cditi (it) stable? ly if rmally use.3
More informationconvection coefficient. The different property values of water at 20 C are given by: u W/m K, h=8062 W/m K
Practice rblems fr Cnvective Heat Transfer 1. Water at 0 C flws ver a flat late 1m 1m at 10 C with a free stream velcity f 4 m/s. Determine the thickness f bndary layers, lcal and average vale f drag cefficient
More informationExamination No. 3 - Tuesday, Nov. 15
NAME (lease rit) SOLUTIONS ECE 35 - DEVICE ELECTRONICS Fall Semester 005 Examiati N 3 - Tuesday, Nv 5 3 4 5 The time fr examiati is hr 5 mi Studets are allwed t use 3 sheets f tes Please shw yur wrk, artial
More informationPipe Networks - Hardy Cross Method Page 1. Pipe Networks
Pie Netwrks - Hardy Crss etd Page Pie Netwrks Itrducti A ie etwrk is a itercected set f ies likig e r mre surces t e r mre demad (delivery) its, ad ca ivlve ay umber f ies i series, bracig ies, ad arallel
More informationENGINEERING COUNCIL CERTIFICATE LEVEL THERMODYNAMIC, FLUID AND PROCESS ENGINEERING C106 TUTORIAL 5 THE VISCOUS NATURE OF FLUIDS
ENGINEERING COUNCIL CERTIFICATE LEVEL THERMODYNAMIC, FLUID AND PROCESS ENGINEERING C106 TUTORIAL 5 THE VISCOUS NATURE OF FLUIDS On cmpletin f this tutrial yu shuld be able t d the fllwing. Define viscsity
More informationrcrit (r C + t m ) 2 ] crit + t o crit The critical radius is evaluated at a given axial location z from the equation + (1 , and D = 4D = 555.
hapter 1 c) When the average bld velcity in the capillary is reduced by a factr f 10, the delivery f the slute t the capillary is liited s that the slute cncentratin after crit 0.018 c is equal t er at
More informationStudy of Energy Eigenvalues of Three Dimensional. Quantum Wires with Variable Cross Section
Adv. Studies Ther. Phys. Vl. 3 009. 5 3-0 Study f Eergy Eigevalues f Three Dimesial Quatum Wires with Variale Crss Secti M.. Sltai Erde Msa Departmet f physics Islamic Aad Uiversity Share-ey rach Ira alrevahidi@yah.cm
More informationShort notes for Heat transfer
Furier s Law f Heat Cnductin Shrt ntes fr Heat transfer Q = Heat transfer in given directin. A = Crss-sectinal area perpendicular t heat flw directin. dt = Temperature difference between tw ends f a blck
More informationMATH Midterm Examination Victor Matveev October 26, 2016
MATH 33- Midterm Examiati Victr Matveev Octber 6, 6. (5pts, mi) Suppse f(x) equals si x the iterval < x < (=), ad is a eve peridic extesi f this fucti t the rest f the real lie. Fid the csie series fr
More informationACTIVE FILTERS EXPERIMENT 2 (EXPERIMENTAL)
EXPERIMENT ATIVE FILTERS (EXPERIMENTAL) OBJETIVE T desig secd-rder lw pass ilters usig the Salle & Key (iite psitive- gai) ad iiite-gai apliier dels. Oe circuit will exhibit a Butterwrth respse ad the
More informationQuantum Mechanics for Scientists and Engineers. David Miller
Quatum Mechaics fr Scietists ad Egieers David Miller Time-depedet perturbati thery Time-depedet perturbati thery Time-depedet perturbati basics Time-depedet perturbati thery Fr time-depedet prblems csider
More information6-5. H 2 O 200 kpa 200 C Q. Entropy Changes of Pure Substances
Canges f ure Substances 6-0C Yes, because an ternally reversible, adiabatic prcess vlves n irreversibilities r eat transfer. 6- e radiatr f a steam eatg system is itially filled wit supereated steam. e
More informationWhat is Uniform flow (normal flow)? Uniform flow means that depth (and velocity) remain constant over a certain reach of the channel.
Hydraulic Lecture # CWR 4 age () Lecture # Outlie: Uiform flow i rectagular cael (age 7-7) Review for tet Aoucemet: Wat i Uiform flow (ormal flow)? Uiform flow mea tat det (ad velocity) remai cotat over
More informationSTRUCTURES IN MIKE 21. Flow over sluice gates A-1
A-1 STRUCTURES IN MIKE 1 Fl ver luice gate Fr a give gemetry f the luice gate ad k ater level uptream ad dtream f the tructure, the fl rate, ca be determied thrugh the equati f eergy ad mmetum - ee B Pedere,
More informationSOLUTION. The reactor thermal output is related to the maximum heat flux in the hot channel by. Z( z ). The position of maximum heat flux ( z max
Te verpwer trip set pit i PWRs is desiged t isure te iu fuel eterlie teperature reais belw a give value T, ad te iiu rati reais abve a give value MR. Fr te give ifrati give a step by step predure, iludig
More informationChapter 3.1: Polynomial Functions
Ntes 3.1: Ply Fucs Chapter 3.1: Plymial Fuctis I Algebra I ad Algebra II, yu ecutered sme very famus plymial fuctis. I this secti, yu will meet may ther members f the plymial family, what sets them apart
More informationare specified , are linearly independent Otherwise, they are linearly dependent, and one is expressed by a linear combination of the others
Chater 3. Higher Order Liear ODEs Kreyszig by YHLee;4; 3-3. Hmgeeus Liear ODEs The stadard frm f the th rder liear ODE ( ) ( ) = : hmgeeus if r( ) = y y y y r Hmgeeus Liear ODE: Suersiti Pricile, Geeral
More informationA L A BA M A L A W R E V IE W
A L A BA M A L A W R E V IE W Volume 52 Fall 2000 Number 1 B E F O R E D I S A B I L I T Y C I V I L R I G HT S : C I V I L W A R P E N S I O N S A N D TH E P O L I T I C S O F D I S A B I L I T Y I N
More informationOE4625 Dredge Pumps and Slurry Transport. Vaclav Matousek October 13, 2004
OE465 Vaclav Matousek October 13, 004 1 Dredge Vermelding Pumps onderdeel and Slurry organisatie Transport OE465 Vaclav Matousek October 13, 004 Dredge Vermelding Pumps onderdeel and Slurry organisatie
More informationInternal Forced Convection. Copyright The McGraw-Hill Companies, Inc. Permission required for reproduction or display.
Internal Forced Convection Copyright The McGraw-Hill Companies, Inc. Permission required for reproduction or display. Introduction Pipe circular cross section. Duct noncircular cross section. Tubes small-diameter
More informationSolutions. Definitions pertaining to solutions
Slutis Defiitis pertaiig t slutis Slute is the substace that is disslved. It is usually preset i the smaller amut. Slvet is the substace that des the disslvig. It is usually preset i the larger amut. Slubility
More informationFundamentals of Heat Transfer Muhammad Rashid Usman
Fundamentals of Heat Transfer Muammad Rasid Usman Institute of Cemical Engineering and Tecnology University of te Punjab, Laore. Figure taken from: ttp://eatexcanger-design.com/20/0/06/eat-excangers-6/
More informationkg m kg kg m =1 slope
(5) Win loa Wen structure blocks te flow of win, te win's kinetic energy is converte into otential energy of ressure, wic causes a win loaing. ensity an velocity of air te angle of incience of te win 3
More informationK E L LY T H O M P S O N
K E L LY T H O M P S O N S E A O LO G Y C R E ATO R, F O U N D E R, A N D PA R T N E R K e l l y T h o m p s o n i s t h e c r e a t o r, f o u n d e r, a n d p a r t n e r o f S e a o l o g y, a n e x
More informationSolution to HW14 Fall-2002
Slutin t HW14 Fall-2002 CJ5 10.CQ.003. REASONING AND SOLUTION Figures 10.11 and 10.14 shw the velcity and the acceleratin, respectively, the shadw a ball that underges unirm circular mtin. The shadw underges
More informationModern Physics. Unit 15: Nuclear Structure and Decay Lecture 15.2: The Strong Force. Ron Reifenberger Professor of Physics Purdue University
Mder Physics Uit 15: Nuclear Structure ad Decay Lecture 15.: The Strg Frce R Reifeberger Prfessr f Physics Purdue Uiversity 1 Bidig eergy er ucle - the deuter Eergy (MeV) ~0.4fm B.E. A =.MeV/ = 1.1 MeV/ucle.
More informationCFD Analysis and Optimization of Heat Transfer in Double Pipe Heat Exchanger with Helical-Tap Inserts at Annulus of Inner Pipe
IOR Journal Mecanical and Civil Engineering (IOR-JMCE) e-in: 2278-1684,p-IN: 2320-334X, Volume 13, Issue 3 Ver. VII (May- Jun. 2016), PP 17-22 www.iosrjournals.org CFD Analysis and Optimization Heat Transfer
More informationPROBLEM 8.3 ( ) p = kg m 1m s m 1000 m = kg s m = bar < P = N m 0.25 m 4 1m s = 1418 N m s = 1.
PROBLEM 8.3 KNOWN: Temperature and velocity of water flow in a pipe of prescribed dimensions. FIND: Pressure drop and pump power requirement for (a) a smooth pipe, (b) a cast iron pipe with a clean surface,
More informationDimensionless Numbers
1 06.10.2017, 09:49 Dimensionless Numbers A. Salih Dept. of Aerospace Engineering IIST, Thiruvananthapuram The nondimensionalization of the governing equations of fluid flow is important for both theoretical
More information"NEET / AIIMS " SOLUTION (6) Avail Video Lectures of Experienced Faculty.
07 NEET EXAMINATION SOLUTION (6) Avail Vide Lectures f Exerienced Faculty Page Sl. The lean exressin which satisfies the utut f this lgic gate is C = A., Whichindicates fr AND gate. We can see, utut C
More informationIf σis unknown. Properties of t distribution. 6.3 One and Two Sample Inferences for Means. What is the correct multiplier? t
/8/009 6.3 Oe a Tw Samle Iferece fr Mea If i kw a 95% Cfiece Iterval i 96 ±.96 96.96 ± But i ever kw. If i ukw Etimate by amle taar eviati The etimate taar errr f the mea will be / Uig the etimate taar
More informationConvection Heat Transfer. Introduction
Convection Heat Transfer Reading Problems 12-1 12-8 12-40, 12-49, 12-68, 12-70, 12-87, 12-98 13-1 13-6 13-39, 13-47, 13-59 14-1 14-4 14-18, 14-24, 14-45, 14-82 Introduction Newton s Law of Cooling Controlling
More informationDifference of 2 kj per mole of propane! E = kj
Ethaly, H Fr rcesses measured uder cstat ressure cditi, the heat the reacti is q. E = q + w = q P ext V he subscrit remids is that the heat measured is uder cstat ressure cditi. hermdyamics Slve r q q
More informationSingle Platform Emitter Location
Sigle Plarm Emier Lcai AOADF FOA Ierermeery TOA SBI LBI Emier Lcai is Tw Esimai Prblems i Oe: Esimae Sigal Parameers a Deed Emier s Lcai: a Time--Arrival TOA Pulses b Pase Ierermeery: Pase is measured
More informationCFD calculation of convective heat transfer coefficients and validation Part I: Laminar flow. Annex 41 Kyoto, April 3 rd to 5 th, 2006
CFD calculation of convective eat transfer coefficients and validation Part I: Laminar flow Annex 41 Kyoto, April 3 rd to 5 t, 2006 Adam Neale 1, Dominique Derome 1, Bert Blocken 2 and Jan Carmeliet 2,3
More information6. Laminar and turbulent boundary layers
6. Laminar and turbulent boundary layers John Richard Thome 8 avril 2008 John Richard Thome (LTCM - SGM - EPFL) Heat transfer - Convection 8 avril 2008 1 / 34 6.1 Some introductory ideas Figure 6.1 A boundary
More informationIn SMV I. IAML: Support Vector Machines II. This Time. The SVM optimization problem. We saw:
In SMV I IAML: Supprt Vectr Machines II Nigel Gddard Schl f Infrmatics Semester 1 We sa: Ma margin trick Gemetry f the margin and h t cmpute it Finding the ma margin hyperplane using a cnstrained ptimizatin
More information[ ] [ ] [ ] [ ] [ ] [ J] dt x x hard to solve in general solve it numerically. If there is no convection. is in the absence of reaction n
.3 The material balance equatin Net change f [J] due t diffusin, cnvectin, and reactin [ ] [ ] [ ] d J J J n = D v k [ J ] fr n - th reactin dt x x hard t slve in general slve it numerically If there is
More informationQ1. A string of length L is fixed at both ends. Which one of the following is NOT a possible wavelength for standing waves on this string?
Term: 111 Thursday, January 05, 2012 Page: 1 Q1. A string f length L is fixed at bth ends. Which ne f the fllwing is NOT a pssible wavelength fr standing waves n this string? Q2. λ n = 2L n = A) 4L B)
More informationUnit code: H/ QCF level: 5 Credit value: 15 OUTCOME 3 - STATIC AND DYNAMIC FLUID SYSTEMS TUTORIAL 3 - VISCOSITY
Unit 43: Plant and Prcess Principles Unit cde: H/601 44 QCF level: 5 Credit value: 15 OUTCOME 3 - STATIC AND DYNAMIC FLUID SYSTEMS TUTORIAL 3 - VISCOSITY 3 Understand static and namic fluid systems with
More informationChapter 8 INTERNAL FORCED CONVECTION
Heat Transfer Chapter 8 INTERNAL FORCED CONVECTION Universitry of Technology Materials Engineering Department MaE216: Heat Transfer and Fluid bjectives Obtain average velocity from a knowledge of velocity
More informationHonors Physics Final Review Summary
Hnrs Physics Final Review Summary Wrk Dne By A Cnstant Frce: Wrk describes a frce s tendency t change the speed f an bject. Wrk is dne nly when an bject mves in respnse t a frce, and a cmpnent f the frce
More informationPhys102 First Major-122 Zero Version Coordinator: Sunaidi Wednesday, March 06, 2013 Page: 1
Crdinatr: Sunaidi Wednesday, March 06, 2013 Page: 1 Q1. An 8.00 m lng wire with a mass f 10.0 g is under a tensin f 25.0 N. A transverse wave fr which the wavelength is 0.100 m, and the amplitude is 3.70
More informationAnalysis of Non-Thermal Equilibrium in Porous Media
Analysis o Non-Thermal Equilibrium in Porous Media A. Nouri-Borujerdi, M. Nazari 1 School o Mechanical Engineering, Shari University o Technology P.O Box 11365-9567, Tehran, Iran E-mail: anouri@shari.edu
More information6. Frequency Response
6. Frequency esnse eading: Sedra & Sith: hater.6, hater 3.6 and hater 9 (MOS rtins, EE 0, Winter 0, F. Najabadi Tyical Frequency resnse an liier U t nw we have ignred the caacitrs. T include the caacitrs,
More informationA) 0.77 N B) 0.24 N C) 0.63 N D) 0.31 N E) 0.86 N. v = ω k = 80 = 32 m/s. Ans: (32) 2 = 0.77 N
Q1. A transverse sinusidal wave travelling n a string is given by: y (x,t) = 0.20 sin (2.5 x 80 t) (SI units). The length f the string is 2.0 m and its mass is 1.5 g. What is the magnitude f the tensin
More informationt r ès s r â 2s ré t s r té s s s s r é é ér t s 2 ï s t 1 s à r
P P r t r t tr t r ès s rs té P rr t r r t t é t q s q é s Prés té t s t r r â 2s ré t s r té s s s s r é é ér t s 2 ï s t 1 s à r ès r é r r t ît P rt ré ré t à r P r s q rt s t t r r2 s rtí 3 Pr ss r
More informationENTROPY GENERATION IN RECTANGULAR DUCTS WITH NONUNIFORM TEMPERATURE ON THE CONTOUR
ENROPY GENERAION IN RECANGULAR UCS WIH NONUNIFORM EMPERAURE ON HE CONOUR Cesar A. Marcelino Matoso Instituto ecnológico de Aeronáutica cesar_matoso@yaoo.ca Ezio Castejon Garcia Instituto ecnológico de
More informationFundamental concept of metal rolling
Fundamental cncept metal rlling Assumptins 1) Te arc cntact between te rlls and te metal is a part a circle. v x x α L p y y R v 2) Te ceicient rictin, µ, is cnstant in tery, but in reality µ varies alng
More informationHeat is energy and is measured in joules (J) or kilojoules (kj). The symbol for heat is H.
Causes f Change Calrimetry Hw Des Energy Affect Change? Heat vs. Temerature HEAT TEMPERATURE Definitin: Deends n: Examles: Heat is energy and is measured in jules (J) r kiljules (kj). The symbl fr heat
More informationAssume that the water in the nozzle is accelerated at a rate such that the frictional effect can be neglected.
1 HW #3: Cnservatin f Linear Mmentum, Cnservatin f Energy, Cnservatin f Angular Mmentum and Turbmachines, Bernulli s Equatin, Dimensinal Analysis, and Pipe Flws Prblem 1. Cnservatins f Mass and Linear
More informationIntroduction to Heat and Mass Transfer. Week 9
Introduction to Heat and Mass Transfer Week 9 補充! Multidimensional Effects Transient problems with heat transfer in two or three dimensions can be considered using the solutions obtained for one dimensional
More informationTable of C on t en t s Global Campus 21 in N umbe r s R e g ional Capac it y D e v e lopme nt in E-L e ar ning Structure a n d C o m p o n en ts R ea
G Blended L ea r ni ng P r o g r a m R eg i o na l C a p a c i t y D ev elo p m ent i n E -L ea r ni ng H R K C r o s s o r d e r u c a t i o n a n d v e l o p m e n t C o p e r a t i o n 3 0 6 0 7 0 5
More informationMANDATORY APPENDIX 41 ELECTRIC IMMERSION HEATER ELEMENT SUPPORT PLATES
41-1 41-5 Page 1 of 5 No changes, age is included for reference. MANDATORY APPENDIX 41 ELECTRIC IMMERSION HEATER ELEMENT SUPPORT PLATES 41-1 SCOPE 41-3 41-1.1 The rules in this Mandatory Aendix cover the
More informationInternal Flow: Heat Transfer in Pipes
Internal Flow: Heat Transfer in Pipes V.Vuorinen Aalto University School of Engineering Heat and Mass Transfer Course, Autumn 2016 November 15 th 2016, Otaniemi ville.vuorinen@aalto.fi First about the
More informationThe Reynolds analogy. 6.6 The Reynolds analogy. The Reynolds analogy. The Reynolds analogy. Turbulence. 6.7 Turbulent boundary layers.
6. ainar and trblent e Reynolds analogy 6.6 e Reynolds analogy Integral oent eq. o lat srace lo itot d d 1 y δ [ ( 1] d δ 6.6 e Reynolds analogy Integral energy eq. or te case o const d d φδ 1 ( y d( δ
More information/ / MET Day 000 NC1^ INRTL MNVR I E E PRE SLEEP K PRE SLEEP R E
05//0 5:26:04 09/6/0 (259) 6 7 8 9 20 2 22 2 09/7 0 02 0 000/00 0 02 0 04 05 06 07 08 09 0 2 ay 000 ^ 0 X Y / / / / ( %/ ) 2 /0 2 ( ) ^ 4 / Y/ 2 4 5 6 7 8 9 2 X ^ X % 2 // 09/7/0 (260) ay 000 02 05//0
More informationPattern Recognition 2014 Support Vector Machines
Pattern Recgnitin 2014 Supprt Vectr Machines Ad Feelders Universiteit Utrecht Ad Feelders ( Universiteit Utrecht ) Pattern Recgnitin 1 / 55 Overview 1 Separable Case 2 Kernel Functins 3 Allwing Errrs (Sft
More informationWork and Heat Definitions
Wrk and eat Deinitins FL- Surrundings: Everything utside system + q -q + System: he part S the rld e are bserving. Wrk, : transer energy as a result unbalanced rces - eat, q: transer energy resulting rm
More informationBasic Fluid Mechanics
Basic Fluid Mechanics Chapter 6A: Internal Incompressible Viscous Flow 4/16/2018 C6A: Internal Incompressible Viscous Flow 1 6.1 Introduction For the present chapter we will limit our study to incompressible
More informationChapter 9 Compressible Flow 667
Chapter 9 Cmpreible Flw 667 9.57 Air flw frm a tank thrugh a nzzle int the tandard atmphere, a in Fig. P9.57. A nrmal hck tand in the exit f the nzzle, a hwn. Etimate (a) the tank preure; and (b) the ma
More informationEE 143 Microfabrication Technology Spring 2010
EE 143 Microfabrication Technology Sring 010 Prof Clark T-C Nguyen Det of Electrical Engineering & Comuter Sciences University of California at Berkeley Berkeley, CA 9470 LecM 5 C Nguyen /14/10 1 Semiconductor
More informationExam in Fluid Mechanics SG2214
Exam in Fluid Mecanics G2214 Final exam for te course G2214 23/10 2008 Examiner: Anders Dalkild Te point value of eac question is given in parentesis and you need more tan 20 points to pass te course including
More informationChapter 10: Flow Flow in in Conduits Conduits Dr Ali Jawarneh
Chater 10: Flow in Conduits By Dr Ali Jawarneh Hashemite University 1 Outline In this chater we will: Analyse the shear stress distribution across a ie section. Discuss and analyse the case of laminar
More informationConvection. forced convection when the flow is caused by external means, such as by a fan, a pump, or atmospheric winds.
Convection The convection heat transfer mode is comprised of two mechanisms. In addition to energy transfer due to random molecular motion (diffusion), energy is also transferred by the bulk, or macroscopic,
More informationConvective Mass Transfer
Convective Mass Transfer Definition of convective mass transfer: The transport of material between a boundary surface and a moving fluid or between two immiscible moving fluids separated by a mobile interface
More informationME 315 Exam 3 8:00-9:00 PM Thursday, April 16, 2009 CIRCLE YOUR DIVISION
ME 315 Exam 3 8:00-9:00 PM Thurday, Aril 16, 009 Thi i a cloed-book, cloed-note examination. There i a formula heet at the back. You mut turn off all communication device before tarting thi exam, and leave
More informationADARSHA H G. EDUSAT PROGRAMME 15 Turbomachines (Unit 3) Axial flow compressors and pumps
EDSA PROGRAMME 5 urbmacines (nit 3) Axial flw cmressrs and ums Axial flw cmressrs and ums are wer absrbing turbmacines. ese macines absrb external wer and tereby increase te entaly f te flwing fluid. Axial
More informationInstruction Sheet COOL SERIES DUCT COOL LISTED H NK O. PR D C FE - Re ove r fro e c sed rea. I Page 1 Rev A
Instruction Sheet COOL SERIES DUCT COOL C UL R US LISTED H NK O you or urc s g t e D C t oroug y e ore s g / as e OL P ea e rea g product PR D C FE RES - Re ove r fro e c sed rea t m a o se e x o duct
More informationAxial Temperature Distribution in W-Tailored Optical Fibers
Axial Temperature Distributi i W-Tailred Optical ibers Mhamed I. Shehata (m.ismail34@yah.cm), Mustafa H. Aly(drmsaly@gmail.cm) OSA Member, ad M. B. Saleh (Basheer@aast.edu) Arab Academy fr Sciece, Techlgy
More informationHEAT TRANSFER BY CONVECTION. Dr. Şaziye Balku 1
HEAT TRANSFER BY CONVECTION Dr. Şaziye Balku 1 CONDUCTION Mechanism of heat transfer through a solid or fluid in the absence any fluid motion. CONVECTION Mechanism of heat transfer through a fluid in the
More informationMAT244 - Ordinary Di erential Equations - Summer 2016 Assignment 2 Due: July 20, 2016
MAT244 - Ordinary Di erential Equations - Summer 206 Assignment 2 Due: July 20, 206 Full Name: Student #: Last First Indicate wic Tutorial Section you attend by filling in te appropriate circle: Tut 0
More informationThermodynamics in combustion
Thermodynamics in combustion 2nd ste in toolbox Thermodynamics deals with a equilibrium state and how chemical comosition can be calculated for a system with known atomic or molecular comosition if 2 indeendent
More informationChapter 8 Sections 8.4 through 8.6 Internal Flow: Heat Transfer Correlations. In fully-developed region. Neglect axial conduction
Chapter 8 Sectin 8.4 thrugh 8.6 Internal Flw: Heat Tranfer Crrelatin T v cu p cp ( rt) k r T T k x r r r r r x In fully-develped regin Neglect axial cnductin u ( rt) r x r r r r r x T v T T T T T u r x
More informationAircraft Performance - Drag
Aircraft Perfrmance - Drag Classificatin f Drag Ntes: Drag Frce and Drag Cefficient Drag is the enemy f flight and its cst. One f the primary functins f aerdynamicists and aircraft designers is t reduce
More informationNumerical Heat and Mass Transfer
Master Degree in Mechanical Engineering Numerical Heat and Mass Transfer 15-Convective Heat Transfer Fausto Arpino f.arpino@unicas.it Introduction In conduction problems the convection entered the analysis
More informationTom BLASINGAME Texas A&M U. Slide 1
Fundamenal Fl Lecure 7 The Diffusiviy Equain fr Mulihase Fl Slide 1 Fundamenal Fl Lecure 7 The Diffusiviy Equain fr Mulihase Fl Slide Fundamenal Fl Lecure 7 The Diffusiviy Equain fr Mulihase Fl Slide 3
More informationNPTEL web course on Complex Analysis. A. Swaminathan I.I.T. Roorkee, India. and. V.K. Katiyar I.I.T. Roorkee, India
NPTEL web course on Complex Analysis A. Swaminathan I.I.T. Roorkee, India and V.K. Katiyar I.I.T. Roorkee, India A.Swaminathan and V.K.Katiyar (NPTEL) Complex Analysis 1 / 20 Complex Analysis Module: 10:
More informationEEO 401 Digital Signal Processing Prof. Mark Fowler
EEO 4 Digital Signal Prcessing Pr. ar Fwler DT Filters te Set #2 Reading Assignment: Sect. 5.4 Prais & anlais /29 Ideal LP Filter Put in the signal we want passed. Suppse that ( ) [, ] X π xn [ ] y[ n]
More information7. Basics of Turbulent Flow Figure 1.
1 7. Basics of Turbulent Flow Whether a flow is laminar or turbulent depends of the relative importance of fluid friction (viscosity) and flow inertia. The ratio of inertial to viscous forces is the Reynolds
More informationSurface and Contact Stress
Surface and Cntact Stress The cncept f the frce is fundamental t mechanics and many imprtant prblems can be cast in terms f frces nly, fr example the prblems cnsidered in Chapter. Hwever, mre sphisticated
More informationCHEM Thermodynamics. Change in Gibbs Free Energy, G. Review. Gibbs Free Energy, G. Review
Review Accrding t the nd law f Thermdynamics, a prcess is spntaneus if S universe = S system + S surrundings > 0 Even thugh S system
More informationL a) Calculate the maximum allowable midspan deflection (w o ) critical under which the beam will slide off its support.
ecture 6 Mderately arge Deflectin Thery f Beams Prblem 6-1: Part A: The department f Highways and Public Wrks f the state f Califrnia is in the prcess f imprving the design f bridge verpasses t meet earthquake
More informationCANKAYA UNIVERSITY FACULTY OF ENGINEERING MECHANICAL ENGINEERING DEPARTMENT ME 313 HEAT TRANSFER
CANKAYA UNIVERSITY FACUTY OF ENGINEERING MECHANICA ENGINEERING DEPARTMENT ME 313 HEAT TRANSFER CHAPTER-3 EXAMPES 1) Cnsider a slab f thicness as illustrated in figure belw. A fluid at temperature T 1 with
More informationControl Systems. Controllability and Observability (Chapter 6)
6.53 trl Systems trllaility ad Oservaility (hapter 6) Geeral Framewrk i State-Spae pprah Give a LTI system: x x u; y x (*) The system might e ustale r des t meet the required perfrmae spe. Hw a we imprve
More informationALE 26. Equilibria for Cell Reactions. What happens to the cell potential as the reaction proceeds over time?
Name Chem 163 Secti: Team Number: AL 26. quilibria fr Cell Reactis (Referece: 21.4 Silberberg 5 th editi) What happes t the ptetial as the reacti prceeds ver time? The Mdel: Basis fr the Nerst quati Previusly,
More informationEstimating h Boundary Layer Equations
Estimating h Boundar Laer Equations ChE 0B Before, we just assumed a heat transfer coefficient, but can we estimate them from first rinciles? Look at stead laminar flow ast a flat late, again: Clearl,
More informationFanno Flow. Gas Dynamics
Fanno Flow Simple frictional flow ( Fanno Flow Adiabatic frictional flow in a constant-area duct * he Flow of a compressible fluid in a duct is Always accompanied by :- ariation in the cross sectional
More informationINTRODUCTION DEFINITION OF FLUID. U p F FLUID IS A SUBSTANCE THAT CAN NOT SUPPORT SHEAR FORCES OF ANY MAGNITUDE WITHOUT CONTINUOUS DEFORMATION
INTRODUCTION DEFINITION OF FLUID plate solid F at t = 0 t > 0 = F/A plate U p F fluid t 0 t 1 t 2 t 3 FLUID IS A SUBSTANCE THAT CAN NOT SUPPORT SHEAR FORCES OF ANY MAGNITUDE WITHOUT CONTINUOUS DEFORMATION
More informationTurbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing.
Turbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing. Thus, it is very important to form both a conceptual understanding and a quantitative
More informationANALYSIS OF ENTROPY GENERATION IN A CIRCULAR TUBE WITH SHORT LENGTH TWISTED TAPE INSERTS
Proceedings of the th National and 11 th International ISHMT-ASME Heat and Mass Transfer Conference December 8-31, 013, IIT Kharagur, India HMTC13006 ANALYSIS OF ENTROPY GENERATION IN A CIRCULAR TUBE WITH
More informationGoverning Equations for Turbulent Flow
Governing Equations for Turbulent Flow (i) Boundary Layer on a Flat Plate ρu x Re x = = Reynolds Number µ Re Re x =5(10) 5 Re x =10 6 x =0 u/ U = 0.99 層流區域 過渡區域 紊流區域 Thickness of boundary layer The Origin
More informationrate~ If no additional source of holes were present, the excess
DIFFUSION OF CARRIERS Diffusion currents are resent in semiconductor devices which generate a satially non-uniform distribution of carriers. The most imortant examles are the -n junction and the biolar
More informationHydraulic validation of the LHC cold mass heat exchanger tube.
Hydraulic validation o te LHC cold mass eat excanger tube. LHC Project Note 155 1998-07-22 (pilippe.provenaz@cern.c) Pilippe PROVENAZ / LHC-ACR Division Summary Te knowledge o te elium mass low vs. te
More informationMATHEMATICS 9740/01 Paper 1 14 Sep hours
Cadidate Name: Class: JC PRELIMINARY EXAM Higher MATHEMATICS 9740/0 Paper 4 Sep 06 3 hurs Additial Materials: Cver page Aswer papers List f Frmulae (MF5) READ THESE INSTRUCTIONS FIRST Write yur full ame
More informationAE301 Aerodynamics I UNIT A: Fundamental Concepts
AE301 Aerodynamics I UNIT A: Fundamental Concets ROAD MAP... A-1: Engineering Fundamentals Reiew A-: Standard Atmoshere A-3: Goerning Equations of Aerodynamics A-4: Airseed Measurements A-5: Aerodynamic
More informationThe Effect Of MHD On Laminar Mixed Convection Of Newtonian Fluid Between Vertical Parallel Plates Channel
The Effect Of MH On Laminar Mixed Convection Of Newtonian Fluid Between Vertical Parallel Plates Channel Rasul alizadeh,alireza darvish behanbar epartment of Mechanic, Faculty of Engineering Science &
More informationNEURAL NETWORKS. modifications of EBP
NEURAL NETWORKS ELEC 50 and ELEC 60 mdiicatins EBP Bdgan M. Wilamwsi + EBP Errr Bac Pragatin algrithm F { z} z F { z } F n {z} The case with multile ututs The weight increment is a suersitin weight mdiicatins
More informationPart 2: Introduction to Open-Channel Flow SPRING 2005
Part : Introduction to Open-Cannel Flow SPRING 005. Te Froude number. Total ead and specific energy 3. Hydraulic jump. Te Froude Number Te main caracteristics of flows in open cannels are tat: tere is
More information