Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Reference9 articles.
1. On Curved Shock Waves
2. Scherrer, Richard, Wimbrow, William R., and Gowen, Forrest E., Heat Transfer and Boundary-Layer Transition on a Heated 20* Cone at a Mach Number of 1.53, N.A.C.A. R.M. A8L28,1949.
3. Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of Attack
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