Slender Body Theory for Supersonic Unsteady Flow
- 1 April 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (4) , 280-281
- https://doi.org/10.2514/8.2249
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Some Results of Sweptback Wing Structural StudiesJournal of the Aeronautical Sciences, 1951
- The Evaluation of Theoretical Critical Compression in Sandwich PlatesJournal of the Aeronautical Sciences, 1951
- On non-steady motion of slender bodiesAeronautical Quarterly, 1950
- The Anticlastic Curvature of Rectangular Beams and PlatesJournal of the Royal Aeronautical Society, 1950
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949