Article

Heat and Mass Transfer and Physical Gasdynamics
2001. V. 39. № 4. P. 558–566
Borodin A.I.
Numerical solution of a three-dimensional multicomponent viscous shock layer by the method of global iterations
Annotation
The model of viscous shock layer is used to solve the three-dimensional problem on supersonic flow of nonequilibrium-dissociating air past smooth bodies of different shapes at different angles of attack and slip.
Article reference:
Borodin A.I. Numerical solution of a three-dimensional multicomponent viscous shock layer by the method of global iterations, High Temp., 2001. V. 39. № 4. P. 558