Supersonic Flow in the Corner Formed by Two Intersecting Wedges
- 1 May 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (5) , 577-578
- https://doi.org/10.2514/3.49299
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Supersonic Interaction in the Corner of Intersecting Wedges at High Reynolds NumbersAIAA Journal, 1972
- Shock-Capturing, Finite-Difference Approach to Supersonic FlowsJournal of Spacecraft and Rockets, 1971
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971
- UNIFORMLY VALID SECOND-ORDER SOLUTION FOR SUPERSONIC FLOW OVER CRUCIFORM SURFACESAIAA Journal, 1963