Menu Close

Study of the attainable flow topologies in a supersonic blunt trailing edge at various blowing ratios

Authors

Yana Gorbachova, Eusebio Valero, Guillermo Paniagua, Alejandro Martinez-Cava and Bayindir H. Saracoglu

Journal Paper

http://doi.org/10.2514/6.2016-0909

Publisher URL

https://arc.aiaa.org/

Publication date

January 2016

American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.Turbomachinery airfoils operated in the transonic regime experience shock wave systems, typically generated at the trailing edge, a phenomenon that leads to unfavorable pressure perturbations downstream