A data-driven non-intrusive polynomial chaos for performance impact of high subsonic compressor cascades with stagger angle and profile errors

Author:

Guo ZhengtaoORCID,Chu Wuli,Zhang Haoguang

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Impact of geometric variability on axial compressor performance;Garzon;J. Turbomach.,2003

2. Influence of manufacturing tolerances and surface roughness of blades on the performance of turbines;Bammert;J. Eng. Gas Turbines Power,1976

3. The effects of rotor blade thickness and surface finish on the performance of a small axial flow turbine;Roelke;J. Eng. Gas Turbines Power,1983

4. Probabilistic CFD simulation of a high-pressure compressor stage taking manufacturing variability into account;Lange,2010

5. Impact of manufacturing variability and nonaxisymmetry on high-pressure compressor stage performance;Lange;J. Eng. Gas Turbines Power,2012

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