Delta wing shock shape at hypersonic speed
- 1 October 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (10) , 2093-2094
- https://doi.org/10.2514/3.6479
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Shock interaction effect on a flapped delta wing at M equals 8.2AIAA Journal, 1971
- Lower Bounds for the Pressure Jump of the Bow Shock of a Supersonic TransportAeronautical Quarterly, 1970