HIgh Fidelity Modeling of Blade Row Interaction in a Transonic Compressor
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American Institute of Aeronautics and Astronautics
Reference17 articles.
1. PIV Study of Wake-Rotor Interactions in a Transonic Compressor at Various Operating Conditions
2. An Investigation of Wake-Shock Interactions in a Transonic Compressor With Digital Particle Image Velocimetry and Time-Accurate Computational Fluid Dynamics
3. 5Turner, M. G., Gorrell, S. E., and Car, D. Radial Migration of Shed Vortices in a Transonic Rotor Following a Wake Generator: A Comparison Between Time Accurate and Average Passage Approach, ASME Paper GT2005-68776, 2005.
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Analysis and Prediction of Shock-Induced Vortex Circulation in Transonic Compressors;Journal of Turbomachinery;2015-10-06
2. Particle Image Velocimetry Analysis on the Effect of Stator Loading on Transonic Blade-Row Interactions;Journal of Turbomachinery;2012-09-04
3. Investigation of Loss Generation in an Embedded Transonic Fan Stage at Several Gaps Using High-Fidelity, Time-Accurate Computational Fluid Dynamics;Journal of Turbomachinery;2009-09-17
4. PIV Measurements of Blade-Row Interactions in a Transonic Compressor for Various Operating Conditions;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21
5. HIgh Fidelity Modeling of Blade Row Interaction in a Transonic Compressor;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08
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