Unsteady pressure response on a rearward-forced, isolated compressible-cascade vane
Author:
Affiliation:
1. Notre Dame, Univ., IN
2. USAF, Inst. of Technology, Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3228
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1. Thomson, D. "TheNational High Cycle Fatigue (HCF) Program," Third National Turbine Engine High Cycle FatigueConference, Feb.1998.
2. Blade-Row Interaction in an Axial-Flow Subsonic Compressor Stage
3. Near-wake measurement in a rotor/stator axial compressor using slanted hot-wire technique
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