Equipment Fundamentals: Heat Exchangers. Chapter 3

Size: px
Start display at page:

Download "Equipment Fundamentals: Heat Exchangers. Chapter 3"

Transcription

1 Equipment Fundamentals: Heat Exchangers Chapter 3

2 Tpics Equipment heat exchangers Cmbines infrmatin abut fluid flw & heat transfer acrss internal bundaries Cnsideratins When d I need t knw the specifics f the heat exchange cnfiguratin? Hw is the heat transfer cefficient related t the utlet temperatures? What is an apprach temperature? Fundamentals f heat transfer & exchange Heat transfer acrss bundaries Cnductin Cnvectin Radiatin Cupled with internal energy changes Sensible heat effects Phase change 2

3 Tpics Fundamentals f heat transfer & exchange Heat transfer acrss bundaries Cnductin Cnvectin Radiatin Cupled with internal energy changes Sensible heat effects Phase change Area-averaged temperature difference Equipment heat exchangers Cmbines infrmatin abut fluid flw & heat transfer acrss internal bundaries Cnsideratins When d I need t knw the specifics f the heat exchange cnfiguratin? Hw is the heat transfer cefficient related t the utlet temperatures? What is an apprach temperature? 3

4 Fundamentals

5 Heat Transfer Mdes f heat transfer Cnductin Flw f heat thrugh material with n bulk mvement f the material itself Usually thught f thrugh slid, but can als be thrugh a stagnant fluid Fr a flat sld: Q Tht T k A x cld Thrugh a circular pipe: Q 2 L ln D D Thrugh a sphere: i kt ht T 2 Q ktht Tcld 1 1 D D i cld 5

6 Heat Transfer Mdes f heat transfer Cnvectin Flw f heat assciated with fluid mvement natural & frced cnvectin Radiatin Q ht ht T A cld Heat transferred via electrmagnetic radiatin Q A T T 4 4 ht cld 2 2 T ht Tcld Tht Tcld Tht Tcld 6

7 Heat Exchangers Sme Basics Fcus is n the system t have heat flw frm the ht fluid(s) t the cld fluid(s) usually withut direct cntact Use bulk flw parameters t relate the heat cnductin acrss the flw barrier t the change in energy f the ht & cld fluids Accunt fr the series f resistances t heat transfer between the ht & cld fluids Heat exchangers Heat t & frm flwing fluids thrugh impermeable barrier(s) Driving frce fr heat thrugh barriers is the temperature difference between the tw fluids n ppsite sides f the barrier Relate the heat effects in the flwing fluids t the change in enthalpy Often this can be related t the difference in the inlet & utlet temperatures fr the fluids ˆ ˆ Q m Hˆ Hˆ Q m C T T fr cnstant Cˆ Q m Hˆ Hˆ Q m C T T fr cnstant Cˆ H H Hin, Hut, H H ph, Hin, Hut, ph, C C Cut, Cin, C C pc, Cut, Cin, pc, 7

8 Heat Exchangers Sme Basics Relate the heat acrss the barrier t the temperature difference acrss the barrier d Q / L dx TH,in TC,ut U Th Tc Q UA Th Tc AREA AVERAGED It can be shwn that fr many typical cnfiguratins the AREA AVERAGED temperature difference is the LMTD (Lg Mean Temperature Difference) TH(x) TC(x) x TH,ut TC,in where Q UA T T LM LM TH,0 TC,0 TH,1 TC,1 TH ln T T,0 C,0 T H,1 C,1 8

9 Heat Exchangers Sme Basics LMTD is a prescribed calculatin calculating the LMTD frm the prcedure is always crrect. LMTD T 1 ln T T T 1 2 T T T T and limlmtd LMTD is apprpriate fr use as the area averaged temperature difference when temperature vs. heat released/absrbed is a straight line 1-1 c-current & cunter-current flw and Bth ht & cld sides have a cnstant heat r Only pure cmpnent phase change n ne side r the ther (n subcling and/r superheating) 9

10 Heat Transfer Sme Basics Heat exchangers C-Current vs. Cunter-Current vs. Crss-Current flws Cunter-current flw allws the utlet temperatures t apprach mre clsely t the inlet temperature f the ther fluid Crss-current flw is cmplicated & requires knwledge f the actual flw patterns C-Current Cunter-Current Crss-Current Heat exchangers Industrial Heat Exchangers Industrial heat exchangers have a cmbinatin f heat transfer thrugh multiple barriers and a cmbinatin f cunter-current & c-current flw LMTD must be crrected t give the actual area-averaged temperature difference (i.e., driving frce) this is the surce fr ne type f F factr 10

11 Heat Exchanger Example 1 Heat 291,800 lb/hr cld C2+ NGL feed frm 80 F t 105 F using 191,600 lb/hr ht C F Assume nly sensible heat effects Determine C2+ NGL feed heat capacity Btu/lb F C3+ Bttms heat capacity Btu/lb F C3+ Bttms utlet temperature Exchanger duty (UA) fr the exchanger C2+ NGL Feed 291,800 lb/hr 80 F??? F 145 F C3+ Bttms 191,600 lb/hr 240 F 11

12 Heat Exchanger Example 1 Exchanger duty & C3+ Bttms utlet temperature determined frm energy balance arund exchanger T Determinatin f UA requires cnfiguratin infrmatin 1-1 cunter-current flw Q m ˆ ccp, c Tc, ut Tc, in ,353,000 Btu/hr Q Thin F mc ˆ hut,, h p, h T 85.1 F LMTD ln c-current flw T 55.4 F LMTD ln Q Btu UA 157, 000 T 85.1 hr F LMTD Q Btu UA 241, 000 T 55.4 hr F LMTD 12

13 Heat Exchanger Example 1 Determinatin f UA requires cnfiguratin infrmatin 1-2 (1 shell & 2 tube passes) cmbines bth cunter & c-current flw The fluid in the shell pass transfers heat separately t the tw tube banks Ref: GPSA Data Bk, 13 th ed. 13

14 Heat Exchanger Example exchanger calculatins require a cnfiguratin crrectin t relate temperatures t the UA Des nt include crssflw effects acrss the tubes F P R 1ln 1 RP 2 2PR 1 R 1 R 1ln 2 2 PR 1 R 1 Ref: Kern, Prcess Heat Transfer, McGraw-Hill, 1965 Ref: GPSA Data Bk, 13 th ed. 14

15 Heat Exchanger Example exchanger T 85.1 F LMTD ln P R F 0.86 (frm chart) 2 Q UA F T 2 LMTD Btu 182, hr F Ref: GPSA Data Bk, 13 th ed. 15

16 Heat Exchanger Example 1 16

17 Heat Exchanger Example 1 Representatin f temperature prfiles with cmbined flw becmes mre cmplicated. 17

18 Heat Exchanger Example 2 Heat 291,800 lb/hr cld C2+ NGL feed starting frm 80 F using 191,600 lb/hr ht C F. Drive the exchanger t a 10 F apprach temperature Fr 1-1 Cunter-Current flw, what are the utlet temperatures? The C2+ NGL Feed is either heated t 230 F (apprach n the ht inlet side) r the C3+ Bttms is cled t 90 F (apprach n the cld inlet side) Assume nly sensible heat effects Determine C2+ NGL feed heat capacity Btu/lb F C3+ Bttms heat capacity Btu/lb F The utlet temperature that is nt cntrlled by the apprach Exchanger duty (UA) fr the exchanger C2+ NGL Feed 291,800 lb/hr 80 F??? F??? F C3+ Bttms 191,600 lb/hr 240 F 18

19 Heat Exchanger Example 2 Exchanger duty & ther utlet temperature determined frm energy balance arund exchanger If the ht side inlet has the apprach temperature Tcut, Thin, F Qm ˆ ccp, ctc, ut Tc, in ,814,000 Btu/hr Q Thut, Thin, F mc ˆ h This has a temperature crssver this is nt the cntrlling side! If the cld side inlet has the apprach temperature: Thut, Tcin, F Qm ˆ hcp, hth, in Th, ut ,797,000 Btu/hr Q Tcut, Tcin, F mc ˆ c p, h p, c 19

20 Heat Exchanger Example 2 Determinatin f UA fr 1-1 Cunter-Current flw using the cld & ht utlet temperatures f F & 90 F, respectively T 23.0 F LMTD ln Q Btu UA 1, 035, 000 T 23.0 hr F LMTD C2+ NGL Feed 291,800 lb/hr 80 F 90 F F C3+ Bttms 191,600 lb/hr 240 F 20

21 Heat Exchanger Example 3 Heat 291,800 lb/hr cld C2+ NGL feed frm 80 F using 191,600 lb/hr ht C F. 1-1 Cunter-Current heat exchanger frm Example #1 designed with 25% excess heat transfer area (UA=196,000 Btu/hr F) Assume nly sensible heat effects Determine C2+ NGL feed heat capacity Btu/lb F C3+ Bttms heat capacity Btu/lb F Bth utlet temperatures Exchanger duty Need t cuple all three equatins relating heat exchanger duty find the three unknwns C2+ NGL Feed 291,800 lb/hr 80 F??? F??? F C3+ Bttms 191,600 lb/hr 240 F 21

22 Heat Exchanger Example 3 Even thugh it lks like yu ll have t slve the three equatins in an iterative manner, it can be shwn that the heat transfer duty is: T T 1 Hin, Cin, 1 1 Q where exp UA fr m C m C 1 mc C p, C mc H p, H mc mc C p, C H p, H C p, C H p, H S: 1 1 exp Q T Q Thin F mc ˆ h p, h Q Tcin F mc ˆ hut,, T cut,, c p, c 14, 924, 000 Btu/hr C2+ NGL Feed 291,800 lb/hr 80 F F F C3+ Bttms 191,600 lb/hr 240 F 22

23 Heat Exchange with Phase Change Can get significant heat exchange with little t n change in temperature ΔT = 0 ΔT = 340 Ref: GPSA Data Bk, 13 th ed. 23

24 Heat Exchanger Example 4 Cndense 10,000 lb/hr saturated vapr prpane at 120 F using 95 F air. Figure a 10 F apprach temperature, s heat the air up t 110 F. Needed physical prperties Determine Air heat capacity 0.24 Btu/lb F Prpane heat f 120 F 1,236 Btu/lb Exchanger duty Flw rate f air needed Exchanger UA 24

25 Heat Exchanger Example 4 Duty determined frm the prpane energy balance. N sensible heat effect. Q m h vap ,360,000 Btu/hr Air flwrate frm its energy balance: m c Q 12,360,000 3,430,000 lb/hr Cˆ T T pc, cut, cin, Calculate UA knwing the terminal temperatures T 16.4 F LMTD ln Q Btu UA 755, 000 T 16.4 hr F LMTD 25

26 Heat Exchanger Example 4 Calculating the UA is essentially the same as when there is n phase change since the temperature prfiles with heat release are still straight lines. The ht stream s prfile just happens t be a cnstant temperature. 26

27 Heat Exchanger Example 5 Cndense 10,000 lb/hr prpane vapr that is superheated t 160 F (but still with 120 F vapr pressure) using 95 F air heated up t 110 F. Needed physical prperties Determine Air heat capacity 0.24 Btu/lb F Prpane vapr heat capacity 0.52 Btu/lb F Prpane heat f 120 F 1236 Btu/lb Exchanger duty Flw rate f air needed Exchanger UA 27

28 Heat Exchanger Example 5 Duty determined frm the prpane balance. Cmbine sensible heat & latent heat effects Air flwrate frm its energy balance: Q m ˆ h vap Cp, c Th, in Th, BP ,680,000 Btu/hr m c Q 125,680,000 34,900,000 lb/hr Cˆ T T pc, cut, cin, Just using terminal temperatures gives an incrrect result! Q Btu T 36.1 F UA 3, 480, 000 LMTD T 36.1 hr F ln LMTD

29 Heat Exchanger Example 5 Calculating the UA is mre cmplicated than just using the terminal temperatures since there is a drastic break in the temperature prfile fr the cndensing prpane 29

30 Heat Exchanger Example 5 Determine the intermediate air temperature between the sensible & latent heat znes Calculate the UA values fr the tw znes Q T m 123,600,000 Btu/hr cnd h vap Q cnd 123,600,000 Tcin F mc ˆ 34,900, cmid,, p, c T 16.5 F LMTD ln c T 25.0 F LMTD ln Q Btu UA 3, 420, 000 T 36.1 hr F LMTD Q Btu UA 83, 000 T 25.0 hr F LMTD The ttal UA is the sum f these tw cntributins. 30

31 Heat Exchanger Example 6 Can we cndense 10,000 lb/hr prpane vapr that is superheated t 160 F (but still with 120 F vapr pressure) using 95 F air heated up t 140 F? This still gives an apparent 20 F apprach temperature? The answer is NO! It is nt apparent frm the terminal temperatures but there is an internal pinch pint t the temperature prfiles & there wuld be a temperature crssver. The air s utlet temperature is cnstrained by this internal pinch pint. 31

32 Heat Exchanger Example 6 Mre air flw is needed t accmplish this cling. Using a 10 F internal apprach temperature shws that the air s utlet temperature is cnstrained t F. The required air mass flw wuld be calculated accrdingly. 32

33 Heat Transfer Sme Basics Thermal resistances are added when in series Can be cmbined int an verall heat transfer cefficient Acrss a flat plate (i.e., cnstant crss sectinal area) 1 1 L 1 U h k h i Fr radial heat transfer (e.g., thrugh the wall f a tube) must als take int accunt the change is area with respect t radius Overall heat transfer cefficient must als be related t a reference area / diameter 1 1 L 1 UA ha i i kaave ha 1 1 A L A D D D 1 ln U hi Ai k Aave h hi Di k Di h 33

34 Heat Transfer Crrelatins fr Film Cefficients Flw in tubes with n phase change hd D v C NNu NRe NPr p k k When there is a significant difference between wall & bulk fluid b hd D v Cp b NNu NRe NPr w k k w Stirred liquids, heat transfer frm cil frm tank jacket b hd ND C i i p b NNu 0.9 NRe, i NPr 0.9 w k k w b hd ND C i i p b NNu 0.36 NRe, i NPr 0.36 w k k w

35 Typical Overall Heat Transfer Cefficients Heat transfer cefficients are drastically different fr cnditins f biling and/r cndensatin versus when there is sensible heat change. Bubbles break up the films alng the wall Als dependent upn the temperature difference acrss the wall Fundamentals f Natural Gas Prcessing, 2 nd ed., Kidnay, Parrish, & McCartney, 2011 Ref: GPSA Data Bk, 13 th ed. 35

36 Typical Overall Heat Transfer Cefficients Fundamentals f Natural Gas Prcessing, 2 nd ed., Kidnay, Parrish, & McCartney, 2011 Ref: GPSA Data Bk, 13 th ed. 36

37 Typical Fuling Factrs Add these resistances t the reciprcal f the clean verall heat transfer cefficient Ref: GPSA Data Bk, 13 th ed. 37

38 Equipment

39 Gas Prcessing Applicatins Cmmn heat exchangers Shell and Tube Kettle rebiler Aerial clers Plate Frame Plate-Fin (Brazed Aluminum) Hairpin Tank Heaters 39

40 Shell & Tube Heat Exchangers Wrkhrses f the gas prcessing industry Shell side Baffles used in the shell side t minimize channeling Tube side Maniflds allw fr even distributin f fluids int the tubes & cllectin/mixing f fluids ut f the tubes Multiple tube passes make it easier t pull the tube bundle fr maintenance/cleaning and have better allwance fr thermal expansin effects Fig. 3.6, Fundamentals f Natural Gas Prcessing, 2 nd ed., Kidnay, Parrish, & McCartney,

41 Shell and Tube Heat Exchangers (Types) Ref: GPSA Data Bk, 13 th ed. 41

42 Shell and Tube Heat Exchangers (Selectin) Ref: GPSA Data Bk, 13 th ed. 42

43 Kettle Rebiler Shell & tube heat exchanger with the tubes submerged in biling liquid n the shell side Main resistance t heat transfer is n the tube side since biling is ccurring n the shell side Fig. 3.7, Fundamentals f Natural Gas Prcessing, 2 nd ed., Kidnay, Parrish, & McCartney,

44 Plate Frame Heat Exchangers Psitives Lw cst Cmpact high area per weight & vlume Can get very clse apprach temperatures (5 F r lwer) Can be disassembled t clean Negative cnsideratins Limited maximum allwable wrking pressure Susceptible t plugging Fig. 3.9, Fundamentals f Natural Gas Prcessing, 2 nd ed., Kidnay, Parrish, & McCartney,

45 Tank Heaters Integrated int existing equipment (i.e., tanks r vessels) Ref: GPSA Data Bk, 13 th ed. 45

46 Air-Cled Exchangers Fundamentals Air cled exchangers cl fluids with ambient air Seasnal variatin can greatly impact perfrmance Utilize finned tube in increase heat transfer surface area

47 Aerial Clers Fans either push air thrugh (frced draft) r pull air thrugh (induced draft) tube bundle Can cntrl the air flw rate either with a variable speed mtr r with luviers Fig. 3.8, Fundamentals f Natural Gas Prcessing, 2 nd ed., Kidnay, Parrish, & McCartney,

48 Aerial Cler Design Cnsideratins Typically a small number f diameter tubes (e.g., 1in OD) with fins n the air side (e.g., 1/2 r 5/8 in) Design cnsideratins Prcess side pressure drp fr flw inside f tubes Air side Required air flw May need high air flw t prevent temperature crssver, but High air flw gives higher pressure drp & fan pwer Mechanical cnsideratins Ttal number f tubes Tube layut: number f passes, number f rws, pitch Bay size: typically 45 ft X 15 ft max Ref: GPSA Data Bk, 14 th ed. 48

49 Air-Cled Exchangers Types Frced Draft vs. Advantages: Slightly lwer hrsepwer Better maintenance accessibility Easily adaptable fr warm air recirculatin Mst cmmn in gas industry Induced Draft Advantages Better distributin f air Less pssibility f air recirculatin Less effect f sun, rain, r hail Increased capacity in the event f fan failure 49

50 Air-Cled Exchanger Thermal Design ( Temperature CMTD Figs 10-8 & 9) F ~ 1.0 fr 3+ Over/Under Passes

51 Summary

52 Summary Cmmn types f heat exchangers used in the gas prcessing industry Shell & tube Kettle rebiler Air cled exchangers Plate Frame Plate-Fin (Brazed Aluminum) Hairpin Tank Heaters Heat exchange basics Cupling f fluid energy balances with heat transfer acrss barrier Cmmn heat exchanger cnfiguratins Typical heat transfer cefficients Example prcess calculatins invlving heat exchangers 52

53 Supplemental Slides

54 LMTD as Area-Averaged Temperature Difference If the temperature curves are linearly related t the duty then the temperature difference will als be linearly related t duty T T T T T T q dt dq 0 Q Q Can put int differential frm f heat transfer equatin & integrate Q dq U T da d T U T da T T 1 0 dt T T T T T 1 0 d U T T U 1 0 Q T T 1 0 Q da A 0 da T T T T ln T T ln U A QUA UAT T Q T LM 54

55 Shell & Tube Heat Exchangers 55

56 Heat Exchanger Example 7 Heat 291,800 lb/hr cld C2+ NGL feed frm 80 F t 160 F using 191,600 lb/hr ht C F Assume nly sensible heat effects Determine C2+ NGL feed heat capacity Btu/lb F C3+ Bttms heat capacity Btu/lb F C3+ Bttms utlet temperature Exchanger duty (UA) fr the exchanger C2+ NGL Feed 291,800 lb/hr 80 F??? F 145 F C3+ Bttms 191,600 lb/hr 240 F 56

57 Heat Exchanger Example 7 Exchanger duty & C3+ Bttms utlet temperature determined frm energy balance arund exchanger T Determinatin f UA requires cnfiguratin infrmatin 1-1 cunter-current flw Q m ˆ ccp, c Tc, ut Tc, in ,434,000 Btu/hr Q Thin F mc ˆ hut,, h p, h T 67.5 F LMTD ln Q Btu UA 243, 000 T 67.5 hr F LMTD 1-1 c-current flw cannt be dne crssver! 57

58 Heat Exchanger Example exchanger T 67.5 F LMTD ln P R F 0.51 (frm chart) 2 Q UA F T 2 LMTD Btu 477, hr F Ref: GPSA Data Bk, 13 th ed. 58

59 Heat Exchanger Example 7 Crrectin factr belw 0.8. Try 2-4 exchanger T 67.5 F LMTD ln P R F (frm chart) 2 Q UA F T 2 LMTD Btu 263, hr F Ref: GPSA Data Bk, 13 th ed. 59

60 Cling Twer Principles Evaprative cling (Psychrmetry) Dry Bulb versus Wet Bulb Temperature Cntact dry air with water Saturatin f air (vaprizatin f sme water) takes energy Air is cled belw ambient t Wet Bulb temperature Takes advantage f air belw 100% humidity Wet Bulb MUST be lwer than Dry Bulb temperature 60

61 Cling Twer Principles Evaprative cling (Psychrmetry) Wet bulb and dry bulb data fr varius lcatins arund the wrld Fig

62 Example: Hw cld can yu get? Air temperature: 95 F RH = 65% Temperature with cling twer? Temperature with air cler? Wet bulb=84 F

63 Cling Twers Mechanical Induced Draft

64 Cling Twers Mechanical Frced Draft Twertechinc.cm 64

65 Cling Twers Wet Surface Air Cler 65

66 Heat Exchanger Example 1 Heat 291,800 lb/hr cld C2+ NGL feed frm 80 F t 105 F using 191,600 lb/hr ht C F Assume nly sensible heat effects Determine C2+ NGL feed heat capacity Btu/lb F C3+ Bttms heat capacity Btu/lb F C3+ Bttms utlet temperature Exchanger duty (UA) fr the exchanger Des the flw cnfiguratin in a 1-2 exchanger make a difference? C2+ NGL Feed 291,800 lb/hr 80 F??? F 145 F C3+ Bttms 191,600 lb/hr 240 F 66

67 Heat Exchanger Example 1 Determinatin f UA requires cnfiguratin infrmatin 1-2 (1 shell & 2 tube passes) cmbines bth cunter & c-current flw Fur pssible flw cnfiguratins Ht Stream n Shell Side Cld Stream n Shell Side 67

68 Heat Exchanger Example 1 Fur pssible flw cnfiguratins all have the same exit temperatures but different internal prfiles 68

69 Heat Exchanger Example 7 I thught yu said temperature crssvers weren t pssible???? 69

Heat Transfer Fundamentals & Equipment (Supplemental Chapter 9)

Heat Transfer Fundamentals & Equipment (Supplemental Chapter 9) Heat Transfer Fundamentals & Equipment (Supplemental Chapter 9) Tpics Fundamentals f heat transfer & exchange Heat transfer acrss bundaries Cnductin Cnvectin Radiatin Cupled with internal energy changes

More information

Short notes for Heat transfer

Short 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 information

Study Group Report: Plate-fin Heat Exchangers: AEA Technology

Study Group Report: Plate-fin Heat Exchangers: AEA Technology Study Grup Reprt: Plate-fin Heat Exchangers: AEA Technlgy The prblem under study cncerned the apparent discrepancy between a series f experiments using a plate fin heat exchanger and the classical thery

More information

NAME TEMPERATURE AND HUMIDITY. I. Introduction

NAME TEMPERATURE AND HUMIDITY. I. Introduction NAME TEMPERATURE AND HUMIDITY I. Intrductin Temperature is the single mst imprtant factr in determining atmspheric cnditins because it greatly influences: 1. The amunt f water vapr in the air 2. The pssibility

More information

Chapter 4. Unsteady State Conduction

Chapter 4. Unsteady State Conduction Chapter 4 Unsteady State Cnductin Chapter 5 Steady State Cnductin Chee 318 1 4-1 Intrductin ransient Cnductin Many heat transfer prblems are time dependent Changes in perating cnditins in a system cause

More information

Differentiation Applications 1: Related Rates

Differentiation Applications 1: Related Rates Differentiatin Applicatins 1: Related Rates 151 Differentiatin Applicatins 1: Related Rates Mdel 1: Sliding Ladder 10 ladder y 10 ladder 10 ladder A 10 ft ladder is leaning against a wall when the bttm

More information

CANKAYA UNIVERSITY FACULTY OF ENGINEERING MECHANICAL ENGINEERING DEPARTMENT ME 313 HEAT TRANSFER

CANKAYA 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 information

Process Engineering Thermodynamics E (4 sp) Exam

Process Engineering Thermodynamics E (4 sp) Exam Prcess Engineering Thermdynamics 42434 E (4 sp) Exam 9-3-29 ll supprt material is allwed except fr telecmmunicatin devices. 4 questins give max. 3 pints = 7½ + 7½ + 7½ + 7½ pints Belw 6 questins are given,

More information

Chapter 11: Atmosphere

Chapter 11: Atmosphere Chapter 11: Atmsphere Sectin 1: Atmspheric Basics Objectives 1. Describe the cmpsitin f the atmsphere. 2. Cmpare and cntrast the varius layers f the atmsphere. 3. Identify three methds f transferring energy

More information

Numerical Simulation of the Thermal Resposne Test Within the Comsol Multiphysics Environment

Numerical Simulation of the Thermal Resposne Test Within the Comsol Multiphysics Environment Presented at the COMSOL Cnference 2008 Hannver University f Parma Department f Industrial Engineering Numerical Simulatin f the Thermal Respsne Test Within the Cmsl Multiphysics Envirnment Authr : C. Crradi,

More information

Problem 1 Known: Dimensions and materials of the composition wall, 10 studs each with 2.5m high

Problem 1 Known: Dimensions and materials of the composition wall, 10 studs each with 2.5m high Prblem Knwn: Dimensins and materials f the cmpsitin wall, 0 studs each with.5m high Unknwn:. Thermal resistance assciate with wall when surfaces nrmal t the directin f heat flw are isthermal. Thermal resistance

More information

" 1 = # $H vap. Chapter 3 Problems

 1 = # $H vap. Chapter 3 Problems Chapter 3 rblems rblem At 1 atmsphere pure Ge melts at 1232 K and bils at 298 K. he triple pint ccurs at =8.4x1-8 atm. Estimate the heat f vaprizatin f Ge. he heat f vaprizatin is estimated frm the Clausius

More information

Edexcel GCSE Physics

Edexcel GCSE Physics Edexcel GCSE Physics Tpic 10: Electricity and circuits Ntes (Cntent in bld is fr Higher Tier nly) www.pmt.educatin The Structure f the Atm Psitively charged nucleus surrunded by negatively charged electrns

More information

1. Transformer A transformer is used to obtain the approximate output voltage of the power supply. The output of the transformer is still AC.

1. Transformer A transformer is used to obtain the approximate output voltage of the power supply. The output of the transformer is still AC. PHYSIS 536 Experiment 4: D Pwer Supply I. Intrductin The prcess f changing A t D is investigated in this experiment. An integrated circuit regulatr makes it easy t cnstruct a high-perfrmance vltage surce

More information

Phys101 Final Code: 1 Term: 132 Wednesday, May 21, 2014 Page: 1

Phys101 Final Code: 1 Term: 132 Wednesday, May 21, 2014 Page: 1 Phys101 Final Cde: 1 Term: 1 Wednesday, May 1, 014 Page: 1 Q1. A car accelerates at.0 m/s alng a straight rad. It passes tw marks that are 0 m apart at times t = 4.0 s and t = 5.0 s. Find the car s velcity

More information

SPH3U1 Lesson 06 Kinematics

SPH3U1 Lesson 06 Kinematics PROJECTILE MOTION LEARNING GOALS Students will: Describe the mtin f an bject thrwn at arbitrary angles thrugh the air. Describe the hrizntal and vertical mtins f a prjectile. Slve prjectile mtin prblems.

More information

TEMPERATURE CONSIDERATIONS FOR SCR CONTROLS

TEMPERATURE CONSIDERATIONS FOR SCR CONTROLS AN 10-18 Applicatin Nte 10-18 PAYNE ENGINEERING TEMPERATURE CONSIDERATIONS FOR SCR CONTROLS q = (h c + h r ) A (T s - T amb ) TEMPERATURE CONSIDERATIONS FOR SCR CONTROLS Thyristr cntrls - mre cmmnly called

More information

AQA GCSE Physics. Topic 7: Magnetism and Electromagnetism. Notes. (Content in bold is for Higher Tier only)

AQA GCSE Physics. Topic 7: Magnetism and Electromagnetism. Notes. (Content in bold is for Higher Tier only) AQA GCSE Physics Tpic 7: Magnetism and Electrmagnetism Ntes (Cntent in bld is fr Higher Tier nly) Magnets - Nrth and Suth Ples - Same Ples repel - Oppsite ples attract Permanent Magnets - Always magnetic,

More information

Chapter Outline 4/28/2014. P-V Work. P-V Work. Isolated, Closed and Open Systems. Exothermic and Endothermic Processes. E = q + w

Chapter Outline 4/28/2014. P-V Work. P-V Work. Isolated, Closed and Open Systems. Exothermic and Endothermic Processes. E = q + w Islated, Clsed and Open Systems 9.1 Energy as a Reactant r a Prduct 9.2 Transferring Heat and Ding Wrk 9.5 Heats f Reactin and Calrimetry 9.6 Hess s Law and Standard Heats f Reactin 9.7 Heats f Reactin

More information

37 Maxwell s Equations

37 Maxwell s Equations 37 Maxwell s quatins In this chapter, the plan is t summarize much f what we knw abut electricity and magnetism in a manner similar t the way in which James Clerk Maxwell summarized what was knwn abut

More information

EE247B/ME218: Introduction to MEMS Design Lecture 7m1: Lithography, Etching, & Doping CTN 2/6/18

EE247B/ME218: Introduction to MEMS Design Lecture 7m1: Lithography, Etching, & Doping CTN 2/6/18 EE247B/ME218 Intrductin t MEMS Design Lecture 7m1 Lithgraphy, Etching, & Dping Dping f Semicnductrs Semicnductr Dping Semicnductrs are nt intrinsically cnductive T make them cnductive, replace silicn atms

More information

Aircraft Performance - Drag

Aircraft 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 information

z = Geometric height (m)

z = Geometric height (m) 13 Z = Geptential height (m) = Lapse rate (6.5 K km -1 ) R = Gas cnstant fr dry air (287 Jkg -1 K) g = Acceleratin f gravity (9.8 ms -2 ) TS = Surface Temperature (K) p = Initial air pressure (Assumptin:

More information

Thermodynamics Partial Outline of Topics

Thermodynamics Partial Outline of Topics Thermdynamics Partial Outline f Tpics I. The secnd law f thermdynamics addresses the issue f spntaneity and invlves a functin called entrpy (S): If a prcess is spntaneus, then Suniverse > 0 (2 nd Law!)

More information

Part One: Heat Changes and Thermochemistry. This aspect of Thermodynamics was dealt with in Chapter 6. (Review)

Part One: Heat Changes and Thermochemistry. This aspect of Thermodynamics was dealt with in Chapter 6. (Review) CHAPTER 18: THERMODYNAMICS AND EQUILIBRIUM Part One: Heat Changes and Thermchemistry This aspect f Thermdynamics was dealt with in Chapter 6. (Review) A. Statement f First Law. (Sectin 18.1) 1. U ttal

More information

Module 4: General Formulation of Electric Circuit Theory

Module 4: General Formulation of Electric Circuit Theory Mdule 4: General Frmulatin f Electric Circuit Thery 4. General Frmulatin f Electric Circuit Thery All electrmagnetic phenmena are described at a fundamental level by Maxwell's equatins and the assciated

More information

Thermodynamics and Equilibrium

Thermodynamics and Equilibrium Thermdynamics and Equilibrium Thermdynamics Thermdynamics is the study f the relatinship between heat and ther frms f energy in a chemical r physical prcess. We intrduced the thermdynamic prperty f enthalpy,

More information

LECTURE 4 THE CONTENTS OF THIS LECTURE ARE AS FOLLOWS: 1.0 INTRODUCTION 2.0 SOURCES OF HEAT IN MINES 3.0 STRATA HEAT

LECTURE 4 THE CONTENTS OF THIS LECTURE ARE AS FOLLOWS: 1.0 INTRODUCTION 2.0 SOURCES OF HEAT IN MINES 3.0 STRATA HEAT LECTURE 4 THE CONTENTS OF THIS LECTURE ARE AS FOLLOWS: 1.0 INTRODUCTION 2.0 SOURCES OF HEAT IN MINES 3.0 STRATA HEAT 3.1 Gethermal Step and Gethermal Gradient 3.2 Thermal Cnductivity f Rcks 3.3 Heat Flux

More information

Lecture 12. Heat Exchangers. Heat Exchangers Chee 318 1

Lecture 12. Heat Exchangers. Heat Exchangers Chee 318 1 Lecture 2 Heat Exchangers Heat Exchangers Chee 38 Heat Exchangers A heat exchanger s used t exchange heat between tw fluds f dfferent temperatures whch are separated by a sld wall. Heat exchangers are

More information

Assume that the water in the nozzle is accelerated at a rate such that the frictional effect can be neglected.

Assume 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 information

Lecture 17: Free Energy of Multi-phase Solutions at Equilibrium

Lecture 17: Free Energy of Multi-phase Solutions at Equilibrium Lecture 17: 11.07.05 Free Energy f Multi-phase Slutins at Equilibrium Tday: LAST TIME...2 FREE ENERGY DIAGRAMS OF MULTI-PHASE SOLUTIONS 1...3 The cmmn tangent cnstructin and the lever rule...3 Practical

More information

Electric Current and Resistance

Electric Current and Resistance Electric Current and Resistance Electric Current Electric current is the rate f flw f charge thrugh sme regin f space The SI unit f current is the ampere (A) 1 A = 1 C / s The symbl fr electric current

More information

Experiment #3. Graphing with Excel

Experiment #3. Graphing with Excel Experiment #3. Graphing with Excel Study the "Graphing with Excel" instructins that have been prvided. Additinal help with learning t use Excel can be fund n several web sites, including http://www.ncsu.edu/labwrite/res/gt/gt-

More information

More Tutorial at

More Tutorial at Answer each questin in the space prvided; use back f page if extra space is needed. Answer questins s the grader can READILY understand yur wrk; nly wrk n the exam sheet will be cnsidered. Write answers,

More information

Phy 212: General Physics II 1 Chapter 18 Worksheet 3/20/2008

Phy 212: General Physics II 1 Chapter 18 Worksheet 3/20/2008 Phy 1: General Physics II 1 hapter 18 rksheet 3/0/008 Thermal Expansin: 1. A wedding ring cmpsed f pure gld (inner diameter = 1.5 x 10 - m) is placed n a persn s finger (diameter = 1.5 x 10 - m). Bth the

More information

OUTCOME 3 - TUTORIAL 1

OUTCOME 3 - TUTORIAL 1 Unit 42: Heat Transfer and Cmbustin Unit cde: K/60/443 QCF level: 5 Credit value: 5 OUTCOME 3 - TUTORIL 3 Heat transfer equipment Recuperatrs: cncentric tube (parallel and cunter flw, crss flw, shell and

More information

2004 AP CHEMISTRY FREE-RESPONSE QUESTIONS

2004 AP CHEMISTRY FREE-RESPONSE QUESTIONS 2004 AP CHEMISTRY FREE-RESPONSE QUESTIONS 6. An electrchemical cell is cnstructed with an pen switch, as shwn in the diagram abve. A strip f Sn and a strip f an unknwn metal, X, are used as electrdes.

More information

ENGINEERING 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 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 information

In Flow Performance Relationship - IPR Curves

In Flow Performance Relationship - IPR Curves In Flw Perfrmance Relatinshi - IPR Curves The Inflw Perfrmance Relatinshi (IPR) fr a well is the relatinshi between the flw rate f the well and the flwing ressure f the well. In single hase flw this is

More information

Design and Analysis of Gas Turbine Blade by Potential Flow Approach

Design and Analysis of Gas Turbine Blade by Potential Flow Approach V. Vijaya kumar et al Int. Jurnal f Engineering Research and Applicatins RESEARCH ARTICLE OPEN ACCESS Design and Analysis f Gas Turbine Blade by Ptential Flw Apprach V. Vijaya Kumar 1, R. Lalitha Narayana

More information

Physics 2B Chapter 23 Notes - Faraday s Law & Inductors Spring 2018

Physics 2B Chapter 23 Notes - Faraday s Law & Inductors Spring 2018 Michael Faraday lived in the Lndn area frm 1791 t 1867. He was 29 years ld when Hand Oersted, in 1820, accidentally discvered that electric current creates magnetic field. Thrugh empirical bservatin and

More information

Advanced Heat and Mass Transfer by Amir Faghri, Yuwen Zhang, and John R. Howell

Advanced Heat and Mass Transfer by Amir Faghri, Yuwen Zhang, and John R. Howell 6.5 Natural Cnvectin in Enclsures Enclsures are finite spaces bunded by walls and filled with fluid. Natural cnvectin in enclsures, als knwn as internal cnvectin, takes place in rms and buildings, furnaces,

More information

Chapter 30. Inductance

Chapter 30. Inductance Chapter 30 nductance 30. Self-nductance Cnsider a lp f wire at rest. f we establish a current arund the lp, it will prduce a magnetic field. Sme f the magnetic field lines pass thrugh the lp. et! be the

More information

Q1. In figure 1, Q = 60 µc, q = 20 µc, a = 3.0 m, and b = 4.0 m. Calculate the total electric force on q due to the other 2 charges.

Q1. In figure 1, Q = 60 µc, q = 20 µc, a = 3.0 m, and b = 4.0 m. Calculate the total electric force on q due to the other 2 charges. Phys10 Secnd Majr-08 Zer Versin Crdinatr: Dr. I. M. Nasser Saturday, May 3, 009 Page: 1 Q1. In figure 1, Q = 60 µc, q = 0 µc, a = 3.0 m, and b = 4.0 m. Calculate the ttal electric frce n q due t the ther

More information

20 Faraday s Law and Maxwell s Extension to Ampere s Law

20 Faraday s Law and Maxwell s Extension to Ampere s Law Chapter 20 Faraday s Law and Maxwell s Extensin t Ampere s Law 20 Faraday s Law and Maxwell s Extensin t Ampere s Law Cnsider the case f a charged particle that is ming in the icinity f a ming bar magnet

More information

convection coefficient. The different property values of water at 20 C are given by: u W/m K, h=8062 W/m K

convection 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 information

CHM112 Lab Graphing with Excel Grading Rubric

CHM112 Lab Graphing with Excel Grading Rubric Name CHM112 Lab Graphing with Excel Grading Rubric Criteria Pints pssible Pints earned Graphs crrectly pltted and adhere t all guidelines (including descriptive title, prperly frmatted axes, trendline

More information

Materials Engineering 272-C Fall 2001, Lecture 7 & 8 Fundamentals of Diffusion

Materials Engineering 272-C Fall 2001, Lecture 7 & 8 Fundamentals of Diffusion Materials Engineering 272-C Fall 2001, Lecture 7 & 8 Fundamentals f Diffusin Diffusin: Transprt in a slid, liquid, r gas driven by a cncentratin gradient (r, in the case f mass transprt, a chemical ptential

More information

General Chemistry II, Unit I: Study Guide (part I)

General Chemistry II, Unit I: Study Guide (part I) 1 General Chemistry II, Unit I: Study Guide (part I) CDS Chapter 14: Physical Prperties f Gases Observatin 1: Pressure- Vlume Measurements n Gases The spring f air is measured as pressure, defined as the

More information

Supporting information

Supporting information Electrnic Supplementary Material (ESI) fr Physical Chemistry Chemical Physics This jurnal is The wner Scieties 01 ydrgen perxide electrchemistry n platinum: twards understanding the xygen reductin reactin

More information

Physics 2010 Motion with Constant Acceleration Experiment 1

Physics 2010 Motion with Constant Acceleration Experiment 1 . Physics 00 Mtin with Cnstant Acceleratin Experiment In this lab, we will study the mtin f a glider as it accelerates dwnhill n a tilted air track. The glider is supprted ver the air track by a cushin

More information

Q1. 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?

Q1. 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 information

General Chemistry II, Unit II: Study Guide (part 1)

General Chemistry II, Unit II: Study Guide (part 1) General Chemistry II, Unit II: Study Guide (part 1) CDS Chapter 21: Reactin Equilibrium in the Gas Phase General Chemistry II Unit II Part 1 1 Intrductin Sme chemical reactins have a significant amunt

More information

AP CHEMISTRY CHAPTER 6 NOTES THERMOCHEMISTRY

AP CHEMISTRY CHAPTER 6 NOTES THERMOCHEMISTRY AP CHEMISTRY CHAPTER 6 NOTES THERMOCHEMISTRY Energy- the capacity t d wrk r t prduce heat 1 st Law f Thermdynamics: Law f Cnservatin f Energy- energy can be cnverted frm ne frm t anther but it can be neither

More information

Chapters 29 and 35 Thermochemistry and Chemical Thermodynamics

Chapters 29 and 35 Thermochemistry and Chemical Thermodynamics Chapters 9 and 35 Thermchemistry and Chemical Thermdynamics 1 Cpyright (c) 011 by Michael A. Janusa, PhD. All rights reserved. Thermchemistry Thermchemistry is the study f the energy effects that accmpany

More information

NEBB-ASHRAE Technical E-Learning Courses

NEBB-ASHRAE Technical E-Learning Courses NEBB-ASHRAE Technical E-Learning Curses If yu re a NEBB certificatin Candidate lking t enhance yur knwledge within a specific area, OR if yu already are a NEBB Certified Prfessinal r Certified Technician

More information

Physics 231 Lecture 31

Physics 231 Lecture 31 Physics 31 Lecture 31 Mi Main pints f tday s lecture: Heat and heat capacity: Q = cmδt Phase transitins and latent heat: Q = LΔm Mechanisms f heat flw. Cnductive heat flw ΔQ kat ( T1 ) H = = Δt L Examples

More information

SMART TESTING BOMBARDIER THOUGHTS

SMART TESTING BOMBARDIER THOUGHTS Bmbardier Inc. u ses filiales. Tus drits réservés. BOMBARDIER THOUGHTS FAA Bmbardier Wrkshp Mntreal 15-18 th September 2015 Bmbardier Inc. u ses filiales. Tus drits réservés. LEVERAGING ANALYSIS METHODS

More information

Power Formulas for Various Energy Resources and Their Application

Power Formulas for Various Energy Resources and Their Application EP@BHS-TOPIC 2: Energy, UNIT2.2: Energy Cnversin and Efficiency Page 1 UNIT 2.2 Energy Cnversin and Efficiency Purpse Once energy resurces are effectively utilized, cnversin t ther frms f energy is necessary

More information

Phys. 344 Ch 7 Lecture 8 Fri., April. 10 th,

Phys. 344 Ch 7 Lecture 8 Fri., April. 10 th, Phys. 344 Ch 7 Lecture 8 Fri., April. 0 th, 009 Fri. 4/0 8. Ising Mdel f Ferrmagnets HW30 66, 74 Mn. 4/3 Review Sat. 4/8 3pm Exam 3 HW Mnday: Review fr est 3. See n-line practice test lecture-prep is t

More information

NUMBERS, MATHEMATICS AND EQUATIONS

NUMBERS, MATHEMATICS AND EQUATIONS AUSTRALIAN CURRICULUM PHYSICS GETTING STARTED WITH PHYSICS NUMBERS, MATHEMATICS AND EQUATIONS An integral part t the understanding f ur physical wrld is the use f mathematical mdels which can be used t

More information

Page 1 of 13. Helium vessel (Shell) UG-27 UG-28. Bellows Appendix 26 UG-32 UG-33. Head. Head Extension UG-27 UG-28. Helium Outlet UG-27 UG-28

Page 1 of 13. Helium vessel (Shell) UG-27 UG-28. Bellows Appendix 26 UG-32 UG-33. Head. Head Extension UG-27 UG-28. Helium Outlet UG-27 UG-28 JLB-TN-06-07 Renascence Crymdule Intrductin T minimize the hazards assciated with vacuum and pressure lads, sectin 65 in the JLab EH&S manual [] requires dcumentatin f the Renascence crymdule helium vessel

More information

Heat Management Methodology for Successful UV Processing on Heat Sensitive Substrates

Heat Management Methodology for Successful UV Processing on Heat Sensitive Substrates Heat Management Methdlgy fr Successful UV Prcessing n Heat Sensitive Substrates Juliet Midlik Prime UV Systems Abstract: Nw in 2005, UV systems pssess heat management cntrls that fine tune the exthermic

More information

1/2 and e0 e s ' 1+ imm w 4 M s 3 πρ0 r 3 m. n 0 ktr. .Also,since n 0 ktr 1,wehave. 4 3 M sπρ 0 r 3. ktr. 3 M sπρ 0

1/2 and e0 e s ' 1+ imm w 4 M s 3 πρ0 r 3 m. n 0 ktr. .Also,since n 0 ktr 1,wehave. 4 3 M sπρ 0 r 3. ktr. 3 M sπρ 0 Chapter 6 6.1 Shw that fr a very weak slutin drplet (m 4 3 πr3 ρ 0 M s ), (6.8) can be written as e 0 ' 1+ a r b r 3 where a σ 0 /n 0 kt and b imm w / 4 3 M sπρ 0. What is yur interpretatin f thecnd and

More information

THERMAL-VACUUM VERSUS THERMAL- ATMOSPHERIC TESTS OF ELECTRONIC ASSEMBLIES

THERMAL-VACUUM VERSUS THERMAL- ATMOSPHERIC TESTS OF ELECTRONIC ASSEMBLIES PREFERRED RELIABILITY PAGE 1 OF 5 PRACTICES PRACTICE NO. PT-TE-1409 THERMAL-VACUUM VERSUS THERMAL- ATMOSPHERIC Practice: Perfrm all thermal envirnmental tests n electrnic spaceflight hardware in a flight-like

More information

Unit code: H/ QCF level: 5 Credit value: 15 OUTCOME 3 - STATIC AND DYNAMIC FLUID SYSTEMS TUTORIAL 3 - VISCOSITY

Unit 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 information

CHEM Thermodynamics. Change in Gibbs Free Energy, G. Review. Gibbs Free Energy, G. Review

CHEM 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 information

Examiner: Dr. Mohamed Elsharnoby Time: 180 min. Attempt all the following questions Solve the following five questions, and assume any missing data

Examiner: Dr. Mohamed Elsharnoby Time: 180 min. Attempt all the following questions Solve the following five questions, and assume any missing data Benha University Cllege f Engineering at Banha Department f Mechanical Eng. First Year Mechanical Subject : Fluid Mechanics M111 Date:4/5/016 Questins Fr Final Crrective Examinatin Examiner: Dr. Mhamed

More information

FIELD QUALITY IN ACCELERATOR MAGNETS

FIELD QUALITY IN ACCELERATOR MAGNETS FIELD QUALITY IN ACCELERATOR MAGNETS S. Russenschuck CERN, 1211 Geneva 23, Switzerland Abstract The field quality in the supercnducting magnets is expressed in terms f the cefficients f the Furier series

More information

Thermal behavior of Surface Mount Device (SMD) for Spicer case

Thermal behavior of Surface Mount Device (SMD) for Spicer case Thermal behavir f Surface Munt Device (SMD) fr Spicer case Sandip Kumar Saha, Frederik Rgiers, Martine Baelmans sandipkumar.saha@mech.kuleuven.be 3 th Octber 20 Outline Thermal analysis f existing Spicer

More information

bulk velocity through orifice,

bulk velocity through orifice, 150A Review Sessin Other Frictin Lsses Bernulli hf accunts fr all types f drag: is drag due t skin frictin is drag due t fittings (tabulated fractin f the velcity head) is drag due t units (a given r calculated

More information

[COLLEGE ALGEBRA EXAM I REVIEW TOPICS] ( u s e t h i s t o m a k e s u r e y o u a r e r e a d y )

[COLLEGE ALGEBRA EXAM I REVIEW TOPICS] ( u s e t h i s t o m a k e s u r e y o u a r e r e a d y ) (Abut the final) [COLLEGE ALGEBRA EXAM I REVIEW TOPICS] ( u s e t h i s t m a k e s u r e y u a r e r e a d y ) The department writes the final exam s I dn't really knw what's n it and I can't very well

More information

1 The limitations of Hartree Fock approximation

1 The limitations of Hartree Fock approximation Chapter: Pst-Hartree Fck Methds - I The limitatins f Hartree Fck apprximatin The n electrn single determinant Hartree Fck wave functin is the variatinal best amng all pssible n electrn single determinants

More information

CHAPTER Read Chapter 17, sections 1,2,3. End of Chapter problems: 25

CHAPTER Read Chapter 17, sections 1,2,3. End of Chapter problems: 25 CHAPTER 17 1. Read Chapter 17, sectins 1,2,3. End f Chapter prblems: 25 2. Suppse yu are playing a game that uses tw dice. If yu cunt the dts n the dice, yu culd have anywhere frm 2 t 12. The ways f prducing

More information

Revision: August 19, E Main Suite D Pullman, WA (509) Voice and Fax

Revision: August 19, E Main Suite D Pullman, WA (509) Voice and Fax .7.4: Direct frequency dmain circuit analysis Revisin: August 9, 00 5 E Main Suite D Pullman, WA 9963 (509) 334 6306 ice and Fax Overview n chapter.7., we determined the steadystate respnse f electrical

More information

Chapter 23 Electromagnetic Waves Lecture 14

Chapter 23 Electromagnetic Waves Lecture 14 Chapter 23 Electrmagnetic Waves Lecture 14 23.1 The Discvery f Electrmagnetic Waves 23.2 Prperties f Electrmagnetic Waves 23.3 Electrmagnetic Waves Carry Energy and Mmentum 23.4 Types f Electrmagnetic

More information

Lecture 13: Electrochemical Equilibria

Lecture 13: Electrochemical Equilibria 3.012 Fundamentals f Materials Science Fall 2005 Lecture 13: 10.21.05 Electrchemical Equilibria Tday: LAST TIME...2 An example calculatin...3 THE ELECTROCHEMICAL POTENTIAL...4 Electrstatic energy cntributins

More information

Dispersion Ref Feynman Vol-I, Ch-31

Dispersion Ref Feynman Vol-I, Ch-31 Dispersin Ref Feynman Vl-I, Ch-31 n () = 1 + q N q /m 2 2 2 0 i ( b/m) We have learned that the index f refractin is nt just a simple number, but a quantity that varies with the frequency f the light.

More information

AP Physics Heat Transfer and Thermal Expansion

AP Physics Heat Transfer and Thermal Expansion AP Physics Heat Transfer and Thermal Expansin Heat Flw: Heat can flw frm ne system t anther nly if there is a temperature difference between the tw systems. The greater the difference in temperature, the

More information

February 28, 2013 COMMENTS ON DIFFUSION, DIFFUSIVITY AND DERIVATION OF HYPERBOLIC EQUATIONS DESCRIBING THE DIFFUSION PHENOMENA

February 28, 2013 COMMENTS ON DIFFUSION, DIFFUSIVITY AND DERIVATION OF HYPERBOLIC EQUATIONS DESCRIBING THE DIFFUSION PHENOMENA February 28, 2013 COMMENTS ON DIFFUSION, DIFFUSIVITY AND DERIVATION OF HYPERBOLIC EQUATIONS DESCRIBING THE DIFFUSION PHENOMENA Mental Experiment regarding 1D randm walk Cnsider a cntainer f gas in thermal

More information

NATURAL CONVECTION HEAT TRANSFER FROM A HEAT SINK WITH FINS OF DIFFERENT CONFIGURATION

NATURAL CONVECTION HEAT TRANSFER FROM A HEAT SINK WITH FINS OF DIFFERENT CONFIGURATION Internatinal Jurnal f Innvatin and Applied Studies ISSN 2028-9324 Vl. 9 N. 3 Nv. 2014, pp. 1043-1047 2014 Innvative Space f Scientific Research Jurnals http://www.ijias.issr-jurnals.rg/ NATURAL CONVECTION

More information

Types of Gear Pg xxx. Spur Gear Teeth is parallel to axis of rotation Can transmit power between parallel shaft The simplest form for gear

Types of Gear Pg xxx. Spur Gear Teeth is parallel to axis of rotation Can transmit power between parallel shaft The simplest form for gear [Pg / 2] Gears Objectives. 2. 3. 4. 5. Cmpute the frces exerted n gear teeth as they rtate and transmit pwer. Use apprpriate stress analyses t determine the relatinships amng the applied frces, the gemetry

More information

CHAPTER 13 Temperature and Kinetic Theory. Units

CHAPTER 13 Temperature and Kinetic Theory. Units CHAPTER 13 Temperature and Kinetic Thery Units Atmic Thery f Matter Temperature and Thermmeters Thermal Equilibrium and the Zerth Law f Thermdynamics Thermal Expansin Thermal Stress The Gas Laws and Abslute

More information

Chemistry 114 First Hour Exam

Chemistry 114 First Hour Exam Chemistry 114 First Hur Exam Please shw all wrk fr partial credit Name: (4 pints) 1. (12 pints) Espress is made by frcing very ht water under high pressure thrugh finely grund, cmpacted cffee. (Wikipedia)

More information

Matter Content from State Frameworks and Other State Documents

Matter Content from State Frameworks and Other State Documents Atms and Mlecules Mlecules are made f smaller entities (atms) which are bnded tgether. Therefre mlecules are divisible. Miscnceptin: Element and atm are synnyms. Prper cnceptin: Elements are atms with

More information

Spontaneous Processes, Entropy and the Second Law of Thermodynamics

Spontaneous Processes, Entropy and the Second Law of Thermodynamics Chemical Thermdynamics Spntaneus Prcesses, Entrpy and the Secnd Law f Thermdynamics Review Reactin Rates, Energies, and Equilibrium Althugh a reactin may be energetically favrable (i.e. prducts have lwer

More information

Sensible Performance Analysis of Multi-Pass Cross Flow Heat Exchangers

Sensible Performance Analysis of Multi-Pass Cross Flow Heat Exchangers 108, 11002 (2017) DOI: 101051/ mateccnf/201710811002 Sensible Perfrmance nalysis f Multi-Pass Crss Flw Heat Exchangers 1 Karthik Silaipillayarputhur, awfiq l-mughanam 2, bdulelah I l-niniya 2 1 PO Bx 380,

More information

Find this material useful? You can help our team to keep this site up and bring you even more content consider donating via the link on our site.

Find this material useful? You can help our team to keep this site up and bring you even more content consider donating via the link on our site. Find this material useful? Yu can help ur team t keep this site up and bring yu even mre cntent cnsider dnating via the link n ur site. Still having truble understanding the material? Check ut ur Tutring

More information

Preparation work for A2 Mathematics [2017]

Preparation work for A2 Mathematics [2017] Preparatin wrk fr A2 Mathematics [2017] The wrk studied in Y12 after the return frm study leave is frm the Cre 3 mdule f the A2 Mathematics curse. This wrk will nly be reviewed during Year 13, it will

More information

THERMAL TEST LEVELS & DURATIONS

THERMAL TEST LEVELS & DURATIONS PREFERRED RELIABILITY PAGE 1 OF 7 PRACTICES PRACTICE NO. PT-TE-144 Practice: 1 Perfrm thermal dwell test n prtflight hardware ver the temperature range f +75 C/-2 C (applied at the thermal cntrl/munting

More information

Computational modeling techniques

Computational modeling techniques Cmputatinal mdeling techniques Lecture 4: Mdel checing fr ODE mdels In Petre Department f IT, Åb Aademi http://www.users.ab.fi/ipetre/cmpmd/ Cntent Stichimetric matrix Calculating the mass cnservatin relatins

More information

Lecture 02 CSE 40547/60547 Computing at the Nanoscale

Lecture 02 CSE 40547/60547 Computing at the Nanoscale PN Junctin Ntes: Lecture 02 CSE 40547/60547 Cmputing at the Nanscale Letʼs start with a (very) shrt review f semi-cnducting materials: - N-type material: Obtained by adding impurity with 5 valence elements

More information

Weathering. Title: Chemical and Mechanical Weathering. Grade Level: Subject/Content: Earth and Space Science

Weathering. Title: Chemical and Mechanical Weathering. Grade Level: Subject/Content: Earth and Space Science Weathering Title: Chemical and Mechanical Weathering Grade Level: 9-12 Subject/Cntent: Earth and Space Science Summary f Lessn: Students will test hw chemical and mechanical weathering can affect a rck

More information

MODULE 1. e x + c. [You can t separate a demominator, but you can divide a single denominator into each numerator term] a + b a(a + b)+1 = a + b

MODULE 1. e x + c. [You can t separate a demominator, but you can divide a single denominator into each numerator term] a + b a(a + b)+1 = a + b . REVIEW OF SOME BASIC ALGEBRA MODULE () Slving Equatins Yu shuld be able t slve fr x: a + b = c a d + e x + c and get x = e(ba +) b(c a) d(ba +) c Cmmn mistakes and strategies:. a b + c a b + a c, but

More information

A Few Basic Facts About Isothermal Mass Transfer in a Binary Mixture

A Few Basic Facts About Isothermal Mass Transfer in a Binary Mixture Few asic Facts but Isthermal Mass Transfer in a inary Miture David Keffer Department f Chemical Engineering University f Tennessee first begun: pril 22, 2004 last updated: January 13, 2006 dkeffer@utk.edu

More information

22.54 Neutron Interactions and Applications (Spring 2004) Chapter 11 (3/11/04) Neutron Diffusion

22.54 Neutron Interactions and Applications (Spring 2004) Chapter 11 (3/11/04) Neutron Diffusion .54 Neutrn Interactins and Applicatins (Spring 004) Chapter (3//04) Neutrn Diffusin References -- J. R. Lamarsh, Intrductin t Nuclear Reactr Thery (Addisn-Wesley, Reading, 966) T study neutrn diffusin

More information

BASD HIGH SCHOOL FORMAL LAB REPORT

BASD HIGH SCHOOL FORMAL LAB REPORT BASD HIGH SCHOOL FORMAL LAB REPORT *WARNING: After an explanatin f what t include in each sectin, there is an example f hw the sectin might lk using a sample experiment Keep in mind, the sample lab used

More information

( ) kt. Solution. From kinetic theory (visualized in Figure 1Q9-1), 1 2 rms = 2. = 1368 m/s

( ) kt. Solution. From kinetic theory (visualized in Figure 1Q9-1), 1 2 rms = 2. = 1368 m/s .9 Kinetic Mlecular Thery Calculate the effective (rms) speeds f the He and Ne atms in the He-Ne gas laser tube at rm temperature (300 K). Slutin T find the rt mean square velcity (v rms ) f He atms at

More information

Chem 75 February 16, 2017 Exam 2 Solutions

Chem 75 February 16, 2017 Exam 2 Solutions 1. (6 + 6 pints) Tw quick questins: (a) The Handbk f Chemistry and Physics tells us, crrectly, that CCl 4 bils nrmally at 76.7 C, but its mlar enthalpy f vaprizatin is listed in ne place as 34.6 kj ml

More information

ChE 471: LECTURE 4 Fall 2003

ChE 471: LECTURE 4 Fall 2003 ChE 47: LECTURE 4 Fall 003 IDEL RECTORS One f the key gals f chemical reactin engineering is t quantify the relatinship between prductin rate, reactr size, reactin kinetics and selected perating cnditins.

More information