Effects of Inlet Guide Vane Flow Control on Forced Response of a Transonic Fan
The main contributor to the high-cycle fatigue of compressor blades is the response to aerodynamic forcing functions generated by an upstream row of stators or inlet guide vanes. Resonant response to engine order excitation at certain rotor speeds is especially damaging. Studies have shown that fl...
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Virginia Tech
2011
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| Online Access: | http://hdl.handle.net/10919/11056 http://scholar.lib.vt.edu/theses/available/etd-11072003-000400 |