Stability derivatives for bodies of revolution at subsonic speeds
- 1 February 1976
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (2) , 247-250
- https://doi.org/10.2514/3.7078
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Second-order theory for steady or unsteady subsonic flow past slender lifting bodies of finite thickness.AIAA Journal, 1969
- Second-Order Theory for Unsteady Supersonic Flow Past Slender, Pointed Bodies of RevolutionJournal of the Aerospace Sciences, 1960
- Slender-Body Theory-Review and ExtensionJournal of the Aeronautical Sciences, 1953
- The subsonic flow about a body of revolutionQuarterly of Applied Mathematics, 1947