Question: Is outer flow over an airfoil has less camber than the original airfoil?
Options
A : FALSE
B : TRUE
C : -
D : -
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Uniform Flow more questions
Consider a flow over a flat plate of uniform cross....
In steady flow, pathline and stream lines are ___
Is high adverse pressure gradient that occurs at a sharp....
Is lift is generated due to large pressure gradients on....
Is lift loss with increase in angle of attack?
Is thin viscous region forms over the airfoil at low....
What does the below figure show?^
Centre of pressure can be calculated using __
Except at the origin where r=0, the vortex flow is....
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