List of top Aerodynamics Questions

Consider a conventional subsonic fixed-wing airplane. \(e\) is the Oswald efficiency factor and \(AR\) is the aspect ratio. Corresponding to the minimum \(\left(\frac{C_D}{C_L^{3/2}}\right)\), which of the following relations is true?
Across an oblique shock wave in a calorifically perfect gas,
NACA 2412 airfoil has
Consider steady, two-dimensional, incompressible flow over a non-porous flat plate as shown in the figure. For the control volume PQRS, the speed \(u_{\infty}\) at section PQ is uniform and the speed at section RS is given by \(u(y)=A_0\left(\frac{y}{h}\right)^n\), where \(n\) is a positive integer. The value of \(A_0\) for which the flow through section PS will vanish is:
Consider the velocity distribution $u(y)$ shown in the figure. For two adjacent fluid layers L1 and L2, the viscous force exerted by L1 on L2 is _________.