Correlation of Nosetip Boundary-Layer Transition Data Measured in Ballistics-Range Experiments
- 1 March 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (3) , 329-339
- https://doi.org/10.2514/3.50952
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Measurements of Transition-Front Asymmetries on Ablating Graphite Nosetips in Hypersonic FlightAIAA Journal, 1979
- Aerodynamics of ballistic re-entry vehicles with asymmetric nosetipsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Aerodynamics of reentry vehicles with asymmetric nosetip shape changePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Asymmetric nosetip shape change during atmospheric entryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- On the relation between material variability and surface roughnessPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Boundary-Layer Transition Experiments on Pre-Ablated Graphite Nosetips in a Hyperballistics RangeAIAA Journal, 1977
- Transition induced by distributed roughness on blunt bodies in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- The effect of transition and boundary layer development on hypersonic reentry shape changePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Boundary-layer transition at supersonic speeds - Roughness effects with heat transfer.AIAA Journal, 1968
- Boundary-layer transition on blunt bodies - Effect of roughness.AIAA Journal, 1967