LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
- 1 April 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (4) , 794-802
- https://doi.org/10.2514/3.1644
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A Similarity Law for the Normal Force on a Delta Wing at Hypersonic SpeedsJournal of the Aerospace Sciences, 1959