Author:
Schreivogel P.,Paniagua G.,Bottini H.
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering
Reference13 articles.
1. S. Berry, R. Nowak, T. Horvath, Boundary layer control for hypersonic airbreathing vehicles, in: 34th AIAA Fluid Dynamics Conference, no. 2246, AIAA, 2004.
2. M. Borg, S. Schneider, T. Juliano, Effect of Freestream Noise on Roughness-Induced Transition for the X-51A Forebody, Tech. rep., Purdue University, 2008.
3. A.J. Whitehead, Flow-Field and Drag Characteristics of several Boundary-Layer Tripping Elements in Hypersonic Flow, TN D-5454, NASA, 1969.
4. A.M.J. Stone, D.R., Discrete Sonic Jets used as Boundary-Layer Trips at Mach Numbers of 6 and 8.5, Tech. rep., NASA Langley Research Center, 1972.
5. B. Wheaton, S. Schneider, Roughness-induced instability in a laminar boundary layer at Mach 6, in: 48th AIAA Aerospace Science Meeting, no. AIAA Paper 2010-1574, 2010.
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