The Linearized Subsonic and Supersonic Flow About Inclined Slender Bodies of Revolution
- 1 November 1947
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 14 (11) , 631-642
- https://doi.org/10.2514/8.1476
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Exact and Approximate Solutions of Two-Dimensional Oblique Shock FlowJournal of the Aeronautical Sciences, 1947
- Theoretische Einführung in die GasdynamikPublished by Springer Nature ,1943
- Supersonic Flow Over an Inclined Body of RevolutionJournal of the Aeronautical Sciences, 1938