Hypersonic minimum-drag slender bodies of revolution.
- 1 October 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (10) , 1717-1724
- https://doi.org/10.2514/3.3768
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Drag minimization using exact methodsAIAA Journal, 1964
- A STUDY OF SLENDER SHAPES OF MINIMUM DRAG USING THE NEWTON-BUSEMANN PRESSURE COEFFICIENT LAWAIAA Journal, 1963