Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 8959-8966
01.01.2009
8 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Aufsatz (Konferenz)
Englisch
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BOUNDARY LAYER STABILITY ANALYSIS OF THE FREE-PISTON SHOCK TUNNEL HIEST TRANSITION EXPERIMENTS
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