CONTROL VOLUME ANALYSIS OF BOUNDARY LAYER INGESTING PROPULSION SYSTEMS WITH OR WITHOUT SHOCK WAVE AHEAD OF THE INLET
49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL
2011-01-01
11 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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