Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 8959-8966
2009-01-01
8 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
BOUNDARY LAYER STABILITY ANALYSIS OF THE FREE-PISTON SHOCK TUNNEL HIEST TRANSITION EXPERIMENTS
British Library Conference Proceedings | 2010
|