High-Reynolds number boundary-layer shock-wave interaction in transonic flow
- 23 November 2005
- book chapter
- Published by Springer Nature
- p. 149-214
- https://doi.org/10.1007/bfb0021336
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Numerical studies in high Reynolds number aerodynamicsComputers & Fluids, 1980
- The induction driven tunnel T2 at ONERA-CERT - Flow qualities, testing techniques and examples of resultsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Holographic Interferoaietry Applied To The Metrology Of Gaseous FlowsPublished by SPIE-Intl Soc Optical Eng ,1978
- Analytical Theory of Transonic Normal Shock-Turbulent Boundary-Layer InteractionAIAA Journal, 1976
- Supercritical Wing Sections IIPublished by Springer Nature ,1975