Mach Reflection from Overexpanded Nozzle Flows
- 1 September 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (9), 1261-1263
- https://doi.org/10.2514/3.50368
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Hypersonic rarefied flow past the sharp leading edge of a flat plate.AIAA Journal, 1967
- Delta Wings of Shapes Amenable to Exact Shock-wave TheoryJournal of the Royal Aeronautical Society, 1963
- An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric ShapesJournal of the Aerospace Sciences, 1960
- Interaction of Shock WavesReviews of Modern Physics, 1949