Question Tag: Compressible flow
Filter by
Filter by
Questions Per Page:

Velocity potential of a subsonic compressible flow is \[\phi(x,y) = V_{\infty}x + \frac{5}{\sqrt{1 – M_{\infty}^{2}}}e^{2\pi\sqrt{1M_{\infty}^{2}}y}sin2\pi x\] Freestream velocity, pressure and …
 740 views
 1 answers
 0 votes

An airfoil is in airflow with \(0.52\) free stream Mach number. Local Mach number at a given point is \(0.82\). …
 751 views
 1 answers
 0 votes

Calculate the average flow Mach number over AB, assuming that M varies linearly along portion AB inside the expansion wave.The …
 1K views
 1 answers
 0 votes

Calculate the maximum deflection angle through which a sonic flow can be expanded via a centered expansion wave.
 1K views
 1 answers
 0 votes