The influence of transition onset location on the performance of shock control bumps

Publisher: Cambridge University Press

E-ISSN: 2059-6464|117|1196|1037-1051

ISSN: 0001-9240

Source: The Aeronautical Journal, Vol.117, Iss.1196, 2013-10, pp. : 1037-1051

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract