Unified Area Rule for Hypersonic Supersonic Wing-Bodies
- 1 July 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (7) , 961-962
- https://doi.org/10.2514/3.50267
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- A new area rule for hypersonic wing-bodies.AIAA Journal, 1971
- Compressible gas flow through a porous materialInternational Journal of Heat and Mass Transfer, 1971
- Supersonic and hypersonic flow with attached shock waves over delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1971
- Reflections of Weak Shock Waves from Acoustic MaterialsThe Journal of the Acoustical Society of America, 1971
- Non-Darcy Flow Through Fibrous Porous MediaJournal of Applied Mechanics, 1969
- Compressible flow through a porous plateInternational Journal of Heat and Mass Transfer, 1968
- HYPERSONIC AREA RULEAIAA Journal, 1963