Combined effects of mass addition and nose bluntness on boundary-layer transition
- 1 May 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (5) , 857-863
- https://doi.org/10.2514/3.5778
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Unusual boundary-layer transition results on cones in hypersonic flow.AIAA Journal, 1969
- Dynamic stability wind-tunnel tests of a 10 deg cone with simulated ablation at m equals 17.AIAA Journal, 1967
- Shock tunnel investigation of boundary-layer transition at M equals 5.5.AIAA Journal, 1967
- Laminar convective heating and ablation in the Mars atmosphere.AIAA Journal, 1967
- Some effects of roughness and variable entropy on transition at a Mach number of 8Published by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Measurements of Skin Friction of the Compressible Turbulent Boundary Layer on a Cone with Foreign Gas InjectionJournal of the Aerospace Sciences, 1960