Effect of Stagger Angle on the Generation of Entropy in a Low Reynolds Number Compressor Cascade
Author:
Affiliation:
1. Wichita State University
2. Embry-Riddle Aeronautical University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6940
Reference16 articles.
1. The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines
2. Local Measurement of Loss Using Heated Thin-Film Sensors
3. O'Donnell, F.K. and Davies, M.R.D., 2000, "Turbine Blade Entropy Generation Rate Part II: The Measured Loss," ASME paper 2000-GT-0266, ASME Turbo Expo, Munich, Germany.
4. Vaughan, P., April 2000, "Measure the Entropy Generation Rate of a High-pressure Turbine Blade, B.S. Thesis,University of Limerick.
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1. Effects of the Reynolds Number on the Efficiency and Stall Mechanisms in a Three-stage Axial Compressor;Journal of Applied Fluid Mechanics;2024-06-01
2. Comparison of Theoretical and Semi-Empirical Solutions for Dissipation Coefficient in a Low Reynolds Number Compressor Cascade;45th AIAA Fluid Dynamics Conference;2015-06-18
3. Effect of Solidity on the Generation of Entropy in a Low Reynolds Number Compressor Cascade;2013 Aviation Technology, Integration, and Operations Conference;2013-08-08
4. Impact of stagger angle nonuniformity on turbine aerodynamic performance;Journal of Thermal Science;2010-08-28
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