Article

Heat and Mass Transfer and Physical Gasdynamics
2002. V. 40. № 2. P. 228–233
Poplavskaya T.V.
Viscous Shock Layer on a Cone in Hypersonic Flow
Annotation
The results are given of a theoretical investigation of hypersonic flow past a pointed cone at zero angle of attack. The flow characteristics are calculated using equations of complete viscous shock layer. The universal dimensionless dependence of the Stanton number on the determining parameters of the problem is obtained.
Article reference:
Poplavskaya T.V. Viscous Shock Layer on a Cone in Hypersonic Flow, High Temp., 2002. V. 40. № 2. P. 228