Chapter 7 External Forced Convection Flashcards
What does a Nu number of 100 mean
100 x more convection than conduction, 100 x more heat transfer than if fluid was not moving
What is drag
the force a flowing fluid exerts on a body in the flow direction
What makes up lift
components of the pressure and wall shear forces in the normal direction to flow tend to move the body in that direction
What does the drag force depend on
the density of the fluid, the upstream velocity V, the size, shape and orientation of the body among other things
Drag coefficient =
Cd = Fd/ 0.5rhoV^2*A
what is the part of the drag that is due directly to wall shear stress
skin friction drag (or just friction drag)
what is the part of the drag that is due directly to pressure
pressure drag
What is the total drag coefficient equal to
Cd = Cdfriction + Cdpressure
What is most drag due to at low reynolds numbers
friction drag
What is friction drag proportional to
surface area
what is pressure drag proportional to
frontal area and the difference between pressures acting on the front and back of the immersed body
Pressure drag is usually dominant and negligible for what type of bodies
dominant for blunt bodies and negligible for streamlined bodies
When a fluid separates from a body it forms a
separated region between the body and the fluid stream
What happens as the separated region increases
the pressure drag increases
Critical reynolds number for flat plate
5e5, where the distance is from the start of the plate
Local nusselt number for laminar =
isothermal and smooth
0.332 Re(x)^0.5 * Pr ^1/3 for Pr >0.6
Local nusselt number for turbulent=
isothermal and smooth
0.0296 Re(x)^085 * Pr ^1/3 for 0.6<= Pr <= 60 and 5e5 <= Re <= e7
How do the local friction and heat transfer coefficient compare in laminar and turbulent flow
both are higher in turbulent flow
Draw the diagram of convection heat transfer coefficient and local friction coefficients over a flat plate
(isothermal and smooth)
see diagram
Average nusselt number for laminar =
isothermal and smooth
0.664 Re(L)^0.5 * Pr ^1/3 for Re(L) < 5e5
Average nusselt number for turbulent=
isothermal and smooth
0.037 Re(L)^0.8 * Pr ^1/3 for 0.6 < Pr < 60 and 5e5 < Re(L) < e7
Laminar and turbulent Nu
isothermal and smooth
(0.037 Re(L)^0.8 - 871) Pr^1/3 for 0.6 < Pr < 60 and 5e5 < Re(L) < e7
Why do we normally not consider the transition region
as it occurs so quickly we cant see it
What is the peclet number
Pe(x) = Re(x)*Pr