Normal shock wave/turbulent boundary-layer interaction control using ‘smart’ piezoelectric actuators

Publisher： Cambridge University Press

E-ISSN： 2059-6464|109|1101|577-583

ISSN： 0001-9240

Source： The Aeronautical Journal, Vol.109, Iss.1101, 2005-11, pp. : 577-583

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

Related content

Active control of swept shock wave/turbulent boundary-layer interactions

By  

The Aeronautical Journal, Vol. 108, Iss. 1080, 2004-02 ,pp. : 93-101

Cambridge University Press

Access to resources Recommend Favorite

Investigation of active control of swept shock wave/turbulent boundary-layer interactions – PSP results

By  

The Aeronautical Journal, Vol. 108, Iss. 1087, 2004-09 ,pp. : 483-490

Cambridge University Press

Access to resources Recommend Favorite

Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation

By  

The Aeronautical Journal, Vol. 114, Iss. 1155, 2010-05 ,pp. : 299-308

Cambridge University Press

Access to resources Recommend Favorite

Experiments on the hypersonic turbulent shock-wave/boundary-layer interaction and the effects of surface roughness

By  

The Aeronautical Journal, Vol. 109, Iss. 1094, 2005-04 ,pp. : 177-184

Cambridge University Press

Access to resources Recommend Favorite

Numerical simulation of ramp induced shock wave/boundary-layer interaction in turbulent flow

By  

The Aeronautical Journal, Vol. 117, Iss. 1192, 2013-06 ,pp. : 629-638

Cambridge University Press

Access to resources Recommend Favorite