Chapter 7 External Forced Convection Flashcards

1
Q

What does a Nu number of 100 mean

A

100 x more convection than conduction, 100 x more heat transfer than if fluid was not moving

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2
Q

What is drag

A

the force a flowing fluid exerts on a body in the flow direction

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3
Q

What makes up lift

A

components of the pressure and wall shear forces in the normal direction to flow tend to move the body in that direction

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4
Q

What does the drag force depend on

A

the density of the fluid, the upstream velocity V, the size, shape and orientation of the body among other things

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5
Q

Drag coefficient =

A

Cd = Fd/ 0.5rhoV^2*A

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6
Q

what is the part of the drag that is due directly to wall shear stress

A

skin friction drag (or just friction drag)

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7
Q

what is the part of the drag that is due directly to pressure

A

pressure drag

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8
Q

What is the total drag coefficient equal to

A

Cd = Cdfriction + Cdpressure

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9
Q

What is most drag due to at low reynolds numbers

A

friction drag

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10
Q

What is friction drag proportional to

A

surface area

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11
Q

what is pressure drag proportional to

A

frontal area and the difference between pressures acting on the front and back of the immersed body

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12
Q

Pressure drag is usually dominant and negligible for what type of bodies

A

dominant for blunt bodies and negligible for streamlined bodies

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13
Q

When a fluid separates from a body it forms a

A

separated region between the body and the fluid stream

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14
Q

What happens as the separated region increases

A

the pressure drag increases

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15
Q

Critical reynolds number for flat plate

A

5e5, where the distance is from the start of the plate

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16
Q

Local nusselt number for laminar =

isothermal and smooth

A

0.332 Re(x)^0.5 * Pr ^1/3 for Pr >0.6

17
Q

Local nusselt number for turbulent=

isothermal and smooth

A

0.0296 Re(x)^085 * Pr ^1/3 for 0.6<= Pr <= 60 and 5e5 <= Re <= e7

18
Q

How do the local friction and heat transfer coefficient compare in laminar and turbulent flow

A

both are higher in turbulent flow

19
Q

Draw the diagram of convection heat transfer coefficient and local friction coefficients over a flat plate
(isothermal and smooth)

A

see diagram

20
Q

Average nusselt number for laminar =

isothermal and smooth

A

0.664 Re(L)^0.5 * Pr ^1/3 for Re(L) < 5e5

21
Q

Average nusselt number for turbulent=

isothermal and smooth

A

0.037 Re(L)^0.8 * Pr ^1/3 for 0.6 < Pr < 60 and 5e5 < Re(L) < e7

22
Q

Laminar and turbulent Nu

isothermal and smooth

A

(0.037 Re(L)^0.8 - 871) Pr^1/3 for 0.6 < Pr < 60 and 5e5 < Re(L) < e7

23
Q

Why do we normally not consider the transition region

A

as it occurs so quickly we cant see it

24
Q

What is the peclet number

A

Pe(x) = Re(x)*Pr

25
Q

Nu for laminar

flat plate subject to uniform heat flux

A

0.453 Re(x)^0.5 * Pr ^1/3 for Pr > 0.6 Re(x) < 5e5

26
Q

Nu for turbulent

flat plate subject to uniform heat flux

A

0.0308Re(x)^0.8 * Pr ^1/3 for 0.6 < Pr < 60 and 5e5 < Re(L) < e7

27
Q

When heat flux is prescibed the rate of heat transfer to form the plate and the surface temperature at a distance x can be determined from

A

q.s = h(x) (Ts(x) - Tinf)

28
Q

Critical reynolds number for flow across a cylinder or sphere

A

2e5, but laminar boundary layer separation with a turbulent wake flow over a cirular cylinder at 2000

29
Q

What two things are significant for flow over a cylinder or sphere

A

friction and pressure drag

30
Q

Effect of surface roughness on drag coefficient

A

increases it in turbulent flow in general, however for blunt bodeies such a circular clylinder of sphere an increase in surface roughness may increase or decrease the drag coefficient depending on the reynolds number

31
Q

What is it difficult to use an analytical approach to find the heat transfer coefficient of a cylinder or sphere

A

generally involved flow separation which is difficult to analyse, instead several empirical correlations have been developed for the heat transfer coefficient

32
Q

At what temperature are fluid properties evaluated for when calculating Nu over a cylinder

A

film temperature Tf = 1/2 (Tinf + Ts)