Hypersonic flow over a delta wing of moderate aspect ratio.
- 1 March 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (3) , 555-556
- https://doi.org/10.2514/3.3483
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Three-dimensional perturbations on hypersonic wedge flowAIAA Journal, 1964
- SLENDER WINGS AT HIGH ANGLES OF ATTACK IN HYPERSONIC FLOWSPublished by Elsevier ,1962
- The diffraction of blast. IIProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1950