Higher Order Theory of Curved Shock
- 1 May 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 28 (5), 428-430
- https://doi.org/10.2514/8.9020
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Higher-Order Corrections to Taylor's Solution for Weak, Normal, Shock WavesJournal of the Aerospace Sciences, 1960
- Viscous Aerodynamic Characteristics in Hypersonic Rarefied Gas FlowJournal of the Aerospace Sciences, 1960