Observers Design for Shock Position of Supersonic Inlet Based on Equilibrium Manifold
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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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