Last Updated On [03-11-2023]
With increase in airfoil thickness, the critical Mach number for an airfoil is likely to
(A) decrease.
(B) increase.
(C) remain unchanged.
(D) be undefined.
Question ID - 155625 :- With increase in airfoil thickness, the critical Mach number for an airfoil is likely to
(A) decrease.
(B) increase.
(C) remain unchanged.
(D) be undefined.
With increase in airfoil thickness, the critical Mach number for an airfoil is likely to
(A) decrease.
(B) increase.
(C) remain unchanged.
(D) be undefined.
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Due to a body in potential flow, the velocity at a point $A$ in the flow field is $20 \mathrm{~m} / \mathrm{s}$ while the free stream velocity is only $10 \mathrm{~m} / \mathrm{s}$. The value of coefficient of pressure $\left(\mathrm{C}_{\mathrm{p}}\right)$ at the point $\mathrm{A}$ is__________________
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