Computational and Experimental Evaluation of a Complex Inlet Swirl Pattern Generation System
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-5008
Reference18 articles.
1. Distortion test capabilities for future fighter aircraft engines
2. Sensitivity of Multistage Compressor Performance to Inlet Boundary Conditions
3. A method of distortion pattern synthesis for high response data screening
4. The StreamVane Method: A New Way to Generate Swirl Distortion for Jet Engine Research
5. Stereoscopic PIV measurements in a turbofan engine inlet with tailored swirl distortion
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2. Vortical flow development in round ducts across scales for engine inlet applications;Experiments in Fluids;2019-03-01
3. Pressure Screen – SteamVane Interaction Effects on Downstream Flow Distortion Pattern;2018 Joint Propulsion Conference;2018-07-08
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5. Complex Flow Generation and Development in a Full-Scale Turbofan Inlet;Journal of Engineering for Gas Turbines and Power;2018-05-14
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