Shock predictions in conical nozzles
- 1 August 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (8) , 1554-1556
- https://doi.org/10.2514/3.3206
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
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- Experimental investigation of atomic recombination in a supersonic nozzleJournal of Fluid Mechanics, 1963
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- The mechanism of transition in the wake of a thin flat plate placed parallel to a uniform flowJournal of Fluid Mechanics, 1961
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- Concerning some Solutions of the Boundary Layer Equations in HydrodynamicsMathematical Proceedings of the Cambridge Philosophical Society, 1930