Effects of axisymmetric sonic nozzle geometry on Mach disk characteristics
- 1 January 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (1) , 121-122
- https://doi.org/10.2514/3.7751
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- On the Structure of Jet PlumesAIAA Journal, 1974
- Shock standoff distances and Mach-disk diameters in underexpanded sonic jetsAIAA Journal, 1971
- Mach disk in underexpanded exhaust plumesAIAA Journal, 1971
- On freejet terminal shocksAIAA Journal, 1970
- Observations on jet flows from a two- dimensional, underexpanded, sonic nozzle.AIAA Journal, 1968
- Study of the highly underexpanded sonic jet.AIAA Journal, 1966
- Normal shock location of underexpanded gas- particle jetsAIAA Journal, 1965
- Normal shock location in underexpanded gas and gas-particle jetsAIAA Journal, 1964
- LOCATION OF THE NORMAL SHOCK WAVE IN THE EXHAUST PLUME OF A JETAIAA Journal, 1963
- On the Structure of Jets from Highly Underexpanded Nozzles Into Still AirJournal of the Aerospace Sciences, 1959