Passive venting system for modifying cavity flowfields at supersonicspeeds
- 1 March 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (3) , 374-376
- https://doi.org/10.2514/3.9902
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Numerical Heat Transfer and Fluid FlowPublished by Taylor & Francis ,2018
- Porosity effect on supercritical airfoil drag reduction by shock wave/boundary layer controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Store separation from cavities at supersonic flight speedsJournal of Spacecraft and Rockets, 1983