Investigation of Crossflow Shocks on Delta Wings in Supersonic Flow
- 1 January 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (1) , 85-93
- https://doi.org/10.2514/3.50734
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- A systematic development of the supersonic flow fields over and behind wings and wing-body configurations using a shock-capturing finite-difference approachPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Vortical singularities in conical flow.AIAA Journal, 1967