SHOCK TUNNEL AND NUMERICAL STUDIES OF A LARGE INLET-FUELLED INWARD TURNING AXISYMMETRIC SCRAMJET
18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France
2012-01-01
11 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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Investigation of the Effects of Lateral Cowl Length in an Inward Turning Scramjet Inlet
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