Penny Gap Effect on Performance and Secondary Flowfield in a Compressor Cascade
Author:
Affiliation:
1. Technical University of Dresden, 01062 Dresden, Germany
2. Ruhr-Universität Bochum, 44780 Bochum, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34536
Reference20 articles.
1. Influence of Gap Between Casing and Variable Stator Blade on Axial Compressor Performance
2. Methods of Predicting the Tip Clearance Effects in Axial Flow Turbomachinery
3. Effects of Tip Clearance on Blade Loading in a Planar Cascade of Turbine Blades
4. Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade
5. Impact of Variable-Geometry Stator Hub Leakage in a Low Speed Axial Compressor
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