The Law of Stabilization of the Distribution of Gasdynamic Parameters over Airfoil in a Transonic Flow under Periodic Pulsed Energy Supply Conditions

摘要

The law of stabilization, which was established S.A. Khristianovich, is generalized in case of transonic flow around airfoils with pulsed periodic energy supply. It is established that, under certain conditions, the Mach number distribution and the pressure coefficient distribution over the airfoil surface from the nose to the shock are independent of the amount of energy supplied and the position of the energy supply zone.