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The lift can be calculated accurately using the p...
1.
The lift can be calculated accurately using the pressure distribution assuming an inviscid flow.
A.
False
B.
True
Answer» C.
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Related MCQs
Flow separation causes lift to decrease with increasing angle of attack. This is inconsistent with the thin airfoil theory where the lift curve slope is 2π. This is a contradiction.
Which of the following is not related to flow separation?
A state with flow separation and reducing lift at a high angle of attack is___
The pressure drag in a fully attached flow over an airfoil is zero.
Which of the following is responsible for causing form drag?
The component of viscosity that creates skin- friction drag is_____
Select the unmatched pair.
What is responsible for creating the aerodynamic drag on the airfoil?
The lift can be calculated accurately using the pressure distribution assuming an inviscid flow.
The d’Alembert’s Paradox is concerned with ____
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