NUMERICAL INVESTIGATION OF THE FLOW ANGULARITY EFFECTS OF THE NASA LANGLEY UPWT ON THE ARES I DAC1 0.01-SCALE MODEL
49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL
2011-01-01
30 pages
Includes bibliographical references and index
Conference paper
English
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ARES I AERODYNAMIC TESTING AT THE NASA LANGLEY UNITARY PLAN WIND TUNNEL
British Library Conference Proceedings | 2011
|NTRS | 1999