Artificially Induced Boundary-Layer Transition on Blunt-Slender Cones at Hypersonic Speeds
- 1 July 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 16 (4) , 245-251
- https://doi.org/10.2514/3.57651
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Hydrodynamic Stability and Transition to Turbulence in the Hypersonic Boundary Layer over a Sharp ConePublished by Defense Technical Information Center (DTIC) ,1975
- Recent advances in the performance and testing capabilities of the AEDC-VKF Tunnel F /hotshot/ hypersonic facilityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Investigation of the Effects of Nose Bluntness on Natural and Induced Boundary-Layer Transition on Axisymmetric Bodies in Supersonic FlowPublished by Defense Technical Information Center (DTIC) ,1973
- Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High SpeedsAIAA Journal, 1971
- Supersonic boundary-layer transition - Effects of roughness and freestream disturbancesAIAA Journal, 1971
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flowsJournal of Fluid Mechanics, 1962