Effect of Surface Cooling and Roughness on Transition for the Shuttle Orbiter
- 1 March 1978
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 15 (2) , 113-119
- https://doi.org/10.2514/3.57294
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Numerical Computations of Orbiter Flowfields and Laminar Heating RatesJournal of Spacecraft and Rockets, 1977
- The Relation Between Wall Temperature and the Effect of Roughness on Boundary-Layer TransitionJournal of the Aerospace Sciences, 1961