Experimental and numerical study of unsteady viscous flow due to rotor stator interaction in turbines. II - Simulation, integrated flow fields and interpretation-Reference-Cited by-同舟云学术

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Experimental and numerical study of unsteady viscous flow due to rotor stator interaction in turbines. II - Simulation, integrated flow fields and interpretation

Published:1998-07-13 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Chernobrovkin A.¹,Lakshminarayana B.¹

Affiliation:

1. Pennsylvania State Univ., University Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3596

Reference10 articles.

1. Unsteady Flow Field Due to Nozzle Wake Interaction With the Rotor in an Axial Flow Turbine: Part I—Rotor Passage Flow Field

2. Wake ingestion propulsion benefit

3. Turbulent Wakes in Pressure Gradients

4. Van Zante, D., Adamczyk, J., Strazisar, A., and Okiishi, T., 1997, "Wake Recovery Performance Benefit in a High-Speed Axial Compressor", ASMEpaper 97-GT-535, 1997.

Cited by 1 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. Impact of wake on downstream adjacent rotor in low-speed axial compressor;Journal of Thermal Science;2004-05

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