Stability of axisymmetric boundary layers on sharp cones at hypersonic Mach numbers
- 8 June 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- On the stability of the boundary layer on a transonic swept wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Laminar Boundary Layer Stability Measurements at Mach 7 Including Wall Temperature EffectsPublished by Defense Technical Information Center (DTIC) ,1977
- Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer TransitionAIAA Journal, 1975
- Zusammenhang zwischen ebenen und rotationssymmetrischen Grenzschichten in kompressiblen FlüssigkeitenZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1948