Uncertainty Analysis of Blade Geometric Deviation Affecting Compressor Stability Based on Quantitative Parameters

Author:

Ji Tianyuan,Chu Wuli,Chi Zhidong,Guo Zhengtao,Meng Dejun

Publisher

Elsevier BV

Reference47 articles.

1. Uncertainty quantification on the influence of blade thickness deviation at different rotational speeds based on flow dissipation analysis;T Ji;Phys. Fluids,2023

2. Uncertainty analysis of global and local performance impact of inflow and geometric uncertainties using sparse grid-based non-intrusive polynomial chaos;Z Guo;P. I. Mech. Eng. A-J. Pow,2022

3. Impact of geometric variability on axial compressor performance;V E Garzon;J. Turbomach,2003

4. Arbitrary surface flank milling and flank sam in the design and manufacturing of jet engine fan and compressor airfoils;C Y Wu;Turbo Expo: Power for Land, Sea, and Air,2012

5. Effect of manufacturing deviations on performance of axial flow compressor blading;E Marson;Turbo Expo: Power for Land,1992

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