TRANSIENT GROWTH OF A MACH 5.92 FLAT-PLATE BOUNDARY LAYER
48th, Aerospace sciences meeting; 48th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ; 2010 ; Orlando, FL
2010-01-01
19 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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Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness (TN)
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