First- and Second-Order Theory of Supersonic Flow Past Bodies of Revolution
- 1 March 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (3) , 161-178
- https://doi.org/10.2514/8.1896
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Second Approximation to Supersonic Conical FlowsJournal of the Aeronautical Sciences, 1950
- Study of the boundary layer at supersonic speeds in turbulent flow: Case of the flow along a flat plateQuarterly of Applied Mathematics, 1950
- Vorticity in the Supersonic Flow About Yawing ConesJournal of the Aeronautical Sciences, 1948
- SUPERSONIC FLOW PAST SLENDER BODIES OF REVOLUTION THE SLOPE OF WHOSE MERIDIAN SECTION IS DISCONTINUOUSThe Quarterly Journal of Mechanics and Applied Mathematics, 1948
- SUPERSONIC FLOW PAST SLENDER POINTED BODIES OF REVOLUTION AT YAWThe Quarterly Journal of Mechanics and Applied Mathematics, 1948
- The Linearized Subsonic and Supersonic Flow About Inclined Slender Bodies of RevolutionJournal of the Aeronautical Sciences, 1947
- Supersonic Flow Over an Inclined Body of RevolutionJournal of the Aeronautical Sciences, 1938
- Airfoil Theory for Non-Uniform MotionJournal of the Aeronautical Sciences, 1938