The Three Weak Solution Regimes of Supersonic Conical Flow and Their Impact on Engine Inlets
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
2010-01-01
Conference paper
Electronic Resource
English
THE THREE WEAK SOLUTION REGIMES OF SUPERSONIC CONICAL FLOW AND THEIR IMPACT ON ENGINE INLETS
British Library Conference Proceedings | 2010
|Flow fields in supersonic inlets
NTRS | 1979
|Modular Hypersonic Inlets with Conical Flow
NTIS | 1968
|