Optimal Control of a Turbulent Boundary Layer on a Permeable Cylindrical Surface in a Supersonic Gas Flow.

Autor: Mukhametzyanov, I. R.
Zdroj: Russian Aeronautics; Jan2020, Vol. 63 Issue 1, p67-74, 8p
Abstrakt: The paper deals with the problem of constructing the distribution law of the normal component of injection velocity in a turbulent boundary layer at supersonic flow velocities. The problem is solved using the Dorodnitsyn generalized method of integral relations and the Lagrange formalism. The computational experiments conducted have shown the efficiency of optimal controls in comparison with the uniform law of injection. [ABSTRACT FROM AUTHOR]
Databáze: Complementary Index