Numerical Investigation on Transition of Shock Induced Boundary Layer
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 ; 18021-18027
2009-01-01
7 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Conference paper
English
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Shock tunnel investigation of boundary-layer transition at M = 5.5
Engineering Index Backfile | 1967
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