Shuttle Boundary-Layer Transition Due to Distributed Roughness and Surface Cooling
- 1 September 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 19 (5) , 389-396
- https://doi.org/10.2514/3.62275
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Comparison of correlations of Shuttle boundary-layer transition due to distributed roughnessPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Effect of Surface Cooling and Roughness on Transition for the Shuttle OrbiterJournal of Spacecraft and Rockets, 1978
- Numerical Computations of Orbiter Flowfields and Laminar Heating RatesJournal of Spacecraft and Rockets, 1977
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres)Journal of the Aerospace Sciences, 1962
- The Smallest Height of Roughness Capable of Affecting Boundary-Layer TransitionJournal of the Aerospace Sciences, 1959