Lab 3 Flashcards

1
Q

measuring convective heat transfer coefficients

A

ex. measure the heat transfer rate from an airplane wing with fuel inside

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

parameters: Uinfinity

A

free stream velocity

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

parameters: L

A

characteristic wing length

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

parameters: μ

A

fluid viscosity

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

parameters: p (rho)

A

density

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

parameter: k

A

thermal conductivity

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

parameter: Cp

A

specific heat

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

parameters: relevant temperature

A

ambient and surface

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

dependeent variable

A

convective heat transfer coefficanet h-> q

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

reynolds number

A

Re = pUinfL/u = Uinf L / v = inertial forces/vicous forces

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

critical reynolds number

A

Re ~5x10^5 for a flat plate

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

transition to turbulent flow

A

xc/L = Rexc/ReL
ReL > Rexc

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

trip

A

this influences the flow to transition to turbulent flow

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

momentum (velocity) boundary layer

A

region of flow characterized buy velocity gradient and shear stress

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

laminar flow over a flat plane

A

thickness = 5x/sqrt(Rex)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

turbulent flow over a flat plane

A

thickness = 0.37xRex^-1/5

17
Q

thermal boundary layer thickness

A

flow characterized by temperature gradient and heat flux

18
Q

prandtl number

A

viscosity/thermal diffusivity
pr&raquo_space; 1 thicker momentum BL
pr ~ 1 about equal (gas)
Pr &laquo_space;thicker thermal BL

19
Q

nusselt number

A

Nu = hL/kf

20
Q

laminar flow subject to constant surface temperature

A

Nux = hx/k = 0.322Re^1/2Pr^1/3

21
Q

laminar flow subject to constant surface temperature with average boundary layer results

A

Nu = 0.664 Re^1/2Pr^1/3

22
Q

laminar flow subject to constant surface temperature for constant heat flux

A

Nu = 0.453Re^1/2Pr^1/3
pr>0.6

23
Q

how to measure thermal boundary layer

A

vertical thermal couple

24
Q

how to measure velocity boudnary layer

A

preston probe

25
Q

bernoulli’s equation to get velocity measurment

A

ptotal = pu^2/2 + pstatic
pu^2/2 = pdynamic
u = velocity

26
Q

Local heat transfer coefficient measurement

A

htop = hbottom = h (symetric consfiguration)

27
Q

heat disipated by two heaters

A

qheater = V^2front/Rfront + V^2back/Rback

28
Q

local convection heat flux leaving top and bottom surface

A

q’’ = qheater /2LW

29
Q

local convection heat flux leaving top and bottom surface + radiation

A