9 Berry SA, Daryabeigi K,Wurster K. Boundary layer transition on X-43A. AIAA 2008-3736, 2008
[10]
10 Lau KY. Hypersonic boundary-layer transition: application to high speed vehicle design. Journal of Spacecraft & Rockets, 2008, 45 (2): 176-183
[11]
11 Lau KY. Hypersonic boundary layer transition-application to high speed vehicle design. AIAA 2007-0310, 2007
[12]
12 Ferlemann SM, McClinton CR, Rock KE, et al. HyperX Mach 7 scramjet design, ground test and flight results. AIAA 2005-3322, 2005
[13]
13 Berry SA, Nowak RJ, Horvath TJ. Boundary layer control hypersonic airbreathing vehicles. AIAA 2004-2246, 2004
[14]
14 Berry SA, Michael DiFulvio, Kowalkowski MK, et al. Forced boundary-layer transition on X-43 (Hyper-X) in NASA LaRC 20-inch Mach 6 air tunnel. NASA TM 2000-210316, 2000
[15]
15 Berry SA, Michael DiFulvio, Kowalkowski MK, et al. Forced boundary-layer transition on X-43 (Hyper-X) in NASA LaRC 31-inch Mach 10 air tunnel. NASA TM 2000-210315, 2000
[16]
16 Schneider SP. Hypersonic boundary-layer transition on blunt bodies with roughness. AIAA 2008-0501, 2008
[17]
17 Berry SA, Nowak RJ, Horwath TJ, et al. Boundary layer control for hypersonic airbreathing vehicles. AIAA 2004-2245, 2004
[18]
18 Candler G, Johnson H, Alba C, et al. Analysis of modal growth on the leeward centerplane of the X-51 vehicle. AFRL-RB-WP-TM 2010-3001, 2010
[19]
19 Cockrell CE, Engelund WC, Bittner RD, et al. Integrated aero-propulsive CFD methodology for the Hyper-X flight experiment. AIAA 2000-4010, 2000
[20]
20 Buning PG, Wong TC, Dilley AD, et al. Prediction of the Hyper-X stage separation aerodynamics using CFD. AIAA2000-4009, 2000
[21]
21 Frendi A. On the CFD support for the Hyper-X aerodynamic database. AIAA 99-0885, 1999
[22]
22 Parikh P, Engelund W, Sasan A, et al. Evaluation of a CFD method for aerodynamic database development using the Hyper-X stack configuration. AIAA 2004-5385, 2004
[23]
23 Bakos R. Current hypersonic research in the USA. RTOEN-AVT-150-10, 2008
[24]
24 Marshall LA, Corpening GP, Sherrill R. A chief engineer's view of the NASA's X-43A scramjet flight test. AIAA 2005-3332, 2005
[25]
25 Engelund WC. Hyper-X/X-43A aerodynamics: results from the Mach 7 and Mach 10 scramjet flight test. AIAA2005-3405, 2005
[26]
26 Marshall LA, Bahm C, Corpening GP. Overview with results and lessons learned of the X-43A Mach 10 flight. AIAA 2005-3336, 2005