Roughness effects on boundary-layer transition in a nozzle throat
- 1 March 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (3) , 282-289
- https://doi.org/10.2514/3.7772
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Correlation of nosetip boundary-layer transition data measured in ballistics-range experimentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Effect of wall temperature on a supersonic turbulent boundary layerAIAA Journal, 1978
- Effect of surface roughness on blunt body boundary-layer transitionJournal of Spacecraft and Rockets, 1977
- The effect of transition and boundary layer development on hypersonic reentry shape changePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Nozzle Wall Boundary-Layer Transition and Freestream Disturbances at Mach 5AIAA Journal, 1975
- A Program for Transition ResearchAIAA Journal, 1975
- Mean-flow measurements in an axisymmetric compressible turbulent wake.AIAA Journal, 1968
- The Smallest Height of Roughness Capable of Affecting Boundary-Layer TransitionJournal of the Aerospace Sciences, 1959