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...

Full description

Bibliographic Details
Main Author: Peterson, Marshall Warren
Format: Others
Published: BYU ScholarsArchive 2016
Subjects:
CFD
Online Access:https://scholarsarchive.byu.edu/etd/6384
https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=7384&context=etd