Theory of shock wave interaction with a boundary layer on a moving surface
Abstract
A study is made of the upstream motion of a surface with a velocity that is much less than unity and much greater than Re exp 1/8. It is assumed that the flow can be described by NavierStokes equations, the external flow is supersonic, and Re tends to infinity. A solution to the linearized equation is first obtained using a 'threedeck' scheme, after which a solution is presented for the nonlinear case.
 Publication:

PMTF Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki
 Pub Date:
 October 1990
 Bibcode:
 1990PMTF.........8K
 Keywords:

 Boundary Layer Separation;
 Interactional Aerodynamics;
 Shock Wave Interaction;
 Supersonic Flow;
 Boundary Layer Transition;
 Incompressible Fluids;
 NavierStokes Equation;
 Reynolds Number;
 Fluid Mechanics and Heat Transfer