Implementations of Fourier Methods in CFD to Analyze Distortion Transfer and Generation Through a Transonic Fan
Inlet flow distortion is a non-uniform total pressure, total temperature, or swirl (flow angularity) condition at an aircraft engine inlet. Inlet distortion is a critical consideration in modern fan and compressor design. This is especially true as the industry continues to increase the efficiency a...
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| Format: | Others |
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BYU ScholarsArchive
2016
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| Online Access: | https://scholarsarchive.byu.edu/etd/6384 https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=7384&context=etd |