Approximate Determination of Position of the Sonic Line for a Blunt Body in Hypersonic Flow
- 1 December 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (12), 1485-1486
- https://doi.org/10.2514/8.9880
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Nonequilibrium Vortex Flow in a Dissociating GasJournal of the Aerospace Sciences, 1962
- Pitch-Yaw Stability of a Missile Oscillating in Roll via the Second Method of LyapunovJournal of the Aerospace Sciences, 1962
- Approximate Design of Sharp-Cornered Supersonic NozzlesJournal of the Aerospace Sciences, 1962