Research on Several Approaches for Integrated Passage Design of Compressor

Author:

Li Xin,MENG Tongtong,JI Lucheng

Publisher

Elsevier BV

Reference26 articles.

1. Full blended blade and endwall design of a compressor cascade[J];T T Meng;Chinese Journal of Aeronautics,2021

2. A new appraisal of critical B parameter in compressor aerodynamic instability design[J];H X Zeng;Aerospace Science and Technology,2022

3. Improving the aero-thermal characteristics of turbomachinery cascades[J];M Manna;Journal of Turbomachinery,2003

4. Sweep and dihedral effects in axial-flow turbomachinery[J];Smith Jr;Journal of Basic Engineering,1963

5. Design optimization of a transonic compressor blade with sweep and lean integrated with axial slot casing treatment;B X Lu;Aerospace Science and Technology,2023

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