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
01.01.2011
30 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
ARES I AERODYNAMIC TESTING AT THE NASA LANGLEY UNITARY PLAN WIND TUNNEL
British Library Conference Proceedings | 2011
|NTIS | 1998