Flow calculation for air intake
at high speed
at high speed
In this paper the word is given to flow calculation in 2D air intake (picture 1). The air is compressed and slowed down with 4 shock waves (oblique), from Mach number in cross section 1 to desirable Mach number in cross section 5. Calculation is based on assumption that the walls of the intake are ideally smooth and that there is no friction. Methods used in this calculation are based on basic principles and equations for 2D flow.
