Experimental study of stability and transition of supersonic boundary layer on swept wing at mach number 2-4

MLA

Yu. G. Yermolaev, et al. “Experimental Study of Stability and Transition of Supersonic Boundary Layer on Swept Wing at Mach Number 2-4.” Progress in Flight Physics, June 2013. EBSCOhost, https://doi.org/10.1051/eucass/201305081.

APA

Yu. G. Yermolaev, R. I. Kazantsev, Nikolay Semionov, & Alexander D. Kosinov. (2013). Experimental study of stability and transition of supersonic boundary layer on swept wing at mach number 2-4. Progress in Flight Physics. https://doi.org/10.1051/eucass/201305081

Chicago

Yu. G. Yermolaev, R. I. Kazantsev, Nikolay Semionov, and Alexander D. Kosinov. 2013. “Experimental Study of Stability and Transition of Supersonic Boundary Layer on Swept Wing at Mach Number 2-4.” Progress in Flight Physics, June. doi:10.1051/eucass/201305081.