Particle image velocimetry of vane-rotor interaction in a turbine stage
Author:
Affiliation:
1. Purdue Univ., West Lafayette, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3599
Reference6 articles.
1. Bryanston-Cross, P.J., Towers, C.E., Judge, T.R., Towers D.P.,Harasgama, S.P., and Hopwood, S.T."TheApplication of Particle Image Velocimetry (PIV) in a Short Duration Annular Turbine Cascade,"ASME Paper 91-GT-22J, 1991.
2. Wake Region Measurements of a Highly Three-Dimensional Nozzle Guide Vane Tested at DRA Pyestock Using Particle Image Velocimetry
3. Rotor Blade-to-Blade Measurements Using Particle Image Velocimetry
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3. An Investigation of Surge in a High-Speed Centrifugal Compressor Using Digital PIV;Journal of Turbomachinery;2000-01-01
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