AIAA-2005-1110 EXPERIMENTAL INVESTIGATION OF A THREE-DIMENSIONAL SCRAMJET INLET TESTED IN HIGH ENTHALPY IMPULSE WIND TUNNEL AT MACH 6
17th, International symposium on air breathing engines ; 2005 ; Munich, Germany
01.01.2005
87 pages
Includes bibliographical references and index; Papers on CD-ROM
Aufsatz (Konferenz)
Englisch
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