Supersonic Inlet Dynamics Model Based on Equilibrium Manifold
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
01.01.2006
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Observers Design for Shock Position of Supersonic Inlet Based on Equilibrium Manifold
British Library Conference Proceedings | 2006
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AIAA | 1987
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