Modification of flow-structure interaction in the boundary layer on the laminar airfoil in effect of external and internal acoustic excitation

Author： Szuster J.T.   Wojciechowski J.  

Publisher： Institute of Noise Control Engineering

ISSN： 0736-2935

Source： INTER-NOISE and NOISE-CON Congress and Conference Proceedings, Vol.1997, Iss.4, 1997-08, pp. : 1152-1157

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

Experimental Investigation of the Boundary Layer Transition on a Laminar Airfoil Using Infrared Thermography

By Jelínek Tomáš  

EPJ Web of Conference, Vol. 180, Iss. issue, 2018-06 ,pp. : 02040-02040

Edp Sciences

Access to resources Recommend Favorite

Effect of Turbulent Boundary Layer Flow on Measurement of Acoustic Pressure and Intensity

By Lauchle Gerald C.  

Noise Control Engineering Journal, Vol. 23, Iss. 2, 1984-09 ,pp. : 52-59

Institute of Noise Control Engineering

Access to resources Recommend Favorite

Investigation of Effect of Boundary Layer on Flow Structure Around a Cylinder with a Strip

By  

EPJ Web of Conference, Vol. 92, Iss. issue, 2015-05 ,pp. : 02115-02115

Edp Sciences

Access to resources Recommend Favorite

Acoustic impulses of the strong parallel airfoil-vortex interaction

By Kaminski Witold S.  

INTER-NOISE and NOISE-CON Congress and Conference Proceedings, Vol. 1993, Iss. 3, 1993-08 ,pp. : 1757-1760

Institute of Noise Control Engineering

Access to resources Recommend Favorite

Numerical solution of inviscid and viscous laminar and turbulent flow around the airfoil

By  

EPJ Web of Conference, Vol. 114, Iss. issue, 2016-03 ,pp. : 02109-02109

Edp Sciences

Access to resources Recommend Favorite