Investigation of airfoil clocking and inter-blade-row gaps in axial compressors
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
2. Pratt & Whitney, East Hartford, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3008
Reference25 articles.
1. Performance Improvement Through Indexing of Turbine Airfoils: Part 1 — Experimental Investigation
2. Performance Improvement Through Indexing of Turbine Airfoils: Part 2 — Numerical Simulation
3. Computations of Unsteady Multistage Compressor Flows in a Workstation Environment
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1. A New Influence Mechanism of Clocking Effect in Subsonic Compressor;Applied Sciences;2023-09-07
2. Experimental Study of Stator Clocking Effects in an Axial Compressor;Chinese Journal of Aeronautics;2006-11
3. Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine;Journal of Turbomachinery;2004-07-01
4. Clocking effect in a two-stage compressor with different inter-blade-row gaps;Journal of Thermal Science;2004-02
5. Challenges in Predicting Row Interaction Effects in Axial Turbines (Invited);33rd AIAA Fluid Dynamics Conference and Exhibit;2003-06-23
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