Inverse solution of blunt-body flowfields at large angle of attack.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (6), 1079-1085
- https://doi.org/10.2514/3.4140
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack.AIAA Journal, 1966
- Rotational stagnation point flowJournal of Fluid Mechanics, 1964
- On the Numerical Calculation of Detached Bow Shock Waves in Hypersonic FlowJournal of the Aerospace Sciences, 1958