VISUALIZATION OF UNSTEADY BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL
Congress; 28th, International Council of the Aeronautical Sciences; ICAS 2010 proceedings ; 2012 ; Brisbane, Australia
2012-01-01
ICAS2012-P4.5
Includes bibliographical references and author index; Held in e-store (RMS)
Aufsatz (Konferenz)
Englisch
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