Thickness effect on the force of slender delta wings in hypersonic flow
- 1 March 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (3) , 427-433
- https://doi.org/10.2514/3.2882
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST THE LOWER SURFACE OF A DELTA WINGAIAA Journal, 1963
- LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORYAIAA Journal, 1963
- SLENDER WINGS AT HIGH ANGLES OF ATTACK IN HYPERSONIC FLOWSPublished by Elsevier ,1962
- Shock Layer Structure and Entropy Layers in Hypersonic Conical FlowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1962
- A Similarity Law for the Normal Force on a Delta Wing at Hypersonic SpeedsJournal of the Aerospace Sciences, 1959