Stability Characteristics of Supersonic Natural Laminar Flow Wing Design Concept
暂无分享,去创建一个
[1] Daniel Arnal. Boundary layer transition: Predictions based on linear theory , 1994 .
[2] Kenji Yoshida,et al. Experimental and Numerical Research on Boundary Layer Transition Analysis at Supersonic Speed: JAXA-ONERA Cooperative Research Project (Part 2) , 2013 .
[3] Akira Nishizawa,et al. Transition Measurements on the Natural Laminar Flow Wing at Mach 2 , 2001 .
[4] Kenji Yoshida,et al. Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA , 2009 .
[5] Kenjiro Inagaki,et al. Experimental and numerical analysis of laminar flow control at Mach 1.4 , 1999 .
[6] Clives Leyman. Case Study by Aerospatiale and British Aerospace on the Concorde , 2003 .
[7] D Joslin Ronald,et al. Aircraft Laminar Flow Control , 1998 .