Optimal Tolerance Allocation in Blade Manufacturing by Sensitivity-Based Performance Impact Evaluation
Author:
Affiliation:
1. Zhejiang University, 310027 Hangzhou, People’s Republic of China
2. University of California, Irvine, Irvine, California 92697-3975
Funder
Fundamental Research Funds for the Central Universities of China
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference27 articles.
1. Influences of Manufacturing Tolerances and Surface Roughness of Blades on the Performance of Turbines
2. The Effect of Rotor Blade Thickness and Surface Finish on the Performance of a Small Axial Flow Turbine
3. Impact of Geometric Variability on Axial Compressor Performance
4. New Production Cost-Tolerance Models for Tolerance Synthesis
5. Numerical Investigation of the Influence of Real World Blade Profile Variations on the Aerodynamic Performance of Transonic Nozzle Guide Vanes
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