Effect of Nose Geometry on the Aerothermodynamic Environment of Shuttle Entry Configurations
- 1 May 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (5) , 275-281
- https://doi.org/10.2514/3.62063
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Hypersonic Transitional and Turbulent Flow Studies on a Lifting Entry VehicleJournal of Spacecraft and Rockets, 1972
- Separation Patterns of Boundary Layer over an Inclined Body of RevolutionAIAA Journal, 1972
- A Study of General Three-Dimensional Boundary-Layer Problems by an Exact Numerical MethodAIAA Journal, 1971