Publisher: Cambridge University Press
E-ISSN: 2059-6464|113|1149|683-697
ISSN: 0001-9240
Source: The Aeronautical Journal, Vol.113, Iss.1149, 2009-11, pp. : 683-697
Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.
Abstract
Related content
Sub boundary-layer vortex generators for the control of shock induced separation
The Aeronautical Journal, Vol. 110, Iss. 1106, 2006-04 ,pp. :
Active control of swept shock wave/turbulent boundary-layer interactions
The Aeronautical Journal, Vol. 108, Iss. 1080, 2004-02 ,pp. :
A computational investigation of laminar shock/wave boundary layer interactions
The Aeronautical Journal, Vol. 117, Iss. 1187, 2013-01 ,pp. :