Effect of a Bionic Blade Rib on the Loss Characteristics of a Highly Loaded Compressor Cascade

Author:

Guo Chongjia,Yang Xudong,Han Ji-ang,Zhong Jingjun

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

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4. Shock-wave/boundary-layer interaction control using three-dimensional bumps for transonic wings;Ogawa;AIAA J.,2008

5. Three-dimensional contour bumps for transonic wing drag reduction;Qin;Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.,2008

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