Mach Disk from Underexpanded Axisymmetric Nozzle Flow
- 1 August 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (8) , 1079-1082
- https://doi.org/10.2514/3.49415
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- On the Structure of Jet PlumesAIAA Journal, 1974
- Mach Reflection from Overexpanded Nozzle FlowsAIAA Journal, 1972
- Viscous slipstream flow downstream of a centerline Mach reflectionAIAA Journal, 1971
- Mach disk in underexpanded exhaust plumesAIAA Journal, 1971
- Interaction between primary and secondary streams of supersonic ejector systems and their performance characteristicsAIAA Journal, 1964
- LOCATION OF THE NORMAL SHOCK WAVE IN THE EXHAUST PLUME OF A JETAIAA Journal, 1963
- Triple-Shock-Wave IntersectionsPhysics of Fluids, 1959
- On the Structure of Jets from Highly Underexpanded Nozzles Into Still AirJournal of the Aerospace Sciences, 1959
- Interaction of Shock WavesReviews of Modern Physics, 1949
- Interferometric Studies of Faster than Sound Phenomena. Part II. Analysis of Supersonic Air JetsPhysical Review B, 1949