Loss Mechanisms of High-Turning Supercritical Compressor Cascades
Author:
Affiliation:
1. Gardner Denver, Inc., Peachtree City, Georgia 30269
2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 2406
3. Honda R&D Co., Ltd., Saitama 351-0193, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.30579
Reference27 articles.
1. Development of Controlled Diffusion Airfoils for Multistage Compressor Application
2. Design and Testing of a Controlled Diffusion Airfoil Cascade for Industrial Axial Flow Compressor Application
3. Redesign and Performance Analysis of a Transonic Axial Compressor Stator and Equivalent Plane Cascades With Subsonic Controlled Diffusion Blades
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2. Effect of compound lean blades on separation structures in high loaded compressor cascades under high subsonic condition;Frontiers in Energy Research;2022-09-14
3. Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade;Engineering Applications of Computational Fluid Mechanics;2022-01-20
4. Multipoint design optimization for a controlled diffusion airfoil compressor cascade;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2020-02-10
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