One-Dimensional Dynamic Wake Response in an Isolated Rotor due to Inlet Total Pressure Distortion
An experimental investigation of the wake of a low-speed axial-flow compressor rotor was conducted with and without the presence of steady inlet total pressure distortions. The steady three-dimensional rotor inlet flow was obtained by a five-hole pneumatic pressure probe, while the one-dimensional r...
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Virginia Tech
2011
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| Online Access: | http://hdl.handle.net/10919/9587 http://scholar.lib.vt.edu/theses/available/etd-92798-3849 |