Correlation Technique for Predicting Attached Turbulent Boundary-Layer/FIap Interaction Pressures
- 1 January 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (1) , 9-10
- https://doi.org/10.2514/3.50723
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A detailed study of attached and separated compression corner flowfields in high Reynolds number supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Flare-Induced Interaction Lengths in Supersonic, Turbulent Boundary LayersAIAA Journal, 1976
- Results of a strong interaction, wake-like model of supersonic separated and reattaching turbulent flowsAIAA Journal, 1971
- Theory of exhaust-plume/boundary-layer interactions at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970