Computation of a Supersonic Flow Past an Axisymmetric Nozzle Boattail with Jet Exhaust
- 1 August 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (8) , 869-875
- https://doi.org/10.2514/3.50828
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
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