Shape optimization of transonic compressor blade using quasi-three-dimensional flow physics

Authors :: K. D. Lee
J. Chung
Source :: AIAA Journal. 40:389-391
Publication Year :: 2002
Publisher :: American Institute of Aeronautics and Astronautics (AIAA), 2002.

Subjects :: Physics
Optimal design
Blade (geometry)
Mesh generation
Aerospace Engineering
Shape optimization
Geometry
Mechanics
Static pressure
Three dimensional flow
Gas compressor
Transonic

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