Design of a Total Pressure Distortion Generator for Aircraft Engine Testing
A new method and mechanism for generating non-uniform, or distorted, aircraft engine inlet flow is being developed in order to account for dynamic changes during the creation and propagation of the distortion. Total pressure distortions occur in gas turbine engines when the incoming flow is disturb...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/42807 http://scholar.lib.vt.edu/theses/available/etd-05292002-183227/ |