A Modified Model of the Supersonic Laminar Wake
- 1 December 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 25 (12) , 796-797
- https://doi.org/10.2514/8.7899
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Plastic Stability Theory of Thin ShellsJournal of the Aeronautical Sciences, 1957
- A Creep Buckling HypothesisJournal of the Aeronautical Sciences, 1956
- Base Pressure Studies in Rarefied Supersonic FlowsJournal of the Aeronautical Sciences, 1956
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- Theory and Tests on the Plastic Stability of Plates and ShellsJournal of the Aeronautical Sciences, 1949