Aerodynamic adjoint optimization of turbomachinery with direct control on blade design parameters-Reference-Cited by-同舟云学术

Aerodynamic adjoint optimization of turbomachinery with direct control on blade design parameters

Published:2023-11 Issue:11 Volume:36 Page:119-134
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LI Xin,MENG Tongtong,LI Weiwei,ZHOU Ling,JI Lucheng

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference28 articles.

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2. Veres J. Axial and centrifugal compressor mean line flow analysis method. Proceedings of the 47th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition. Reston: AIAA; 2009. p. AIAA2009-1641.

3. Application of new empirical models based on mathematical statistics in the through-flow analysis;Fei;J Therm Sci,2021

4. Troy J. Design optimization of the first stage fan blade of a low bypass turbofan engine [dissertation]. Daytona Beach: Embry-Riddle Aeronautical University; 2006.

5. Dreyer J, Martinelli L. Hydrodynamic shape optimization of propulsor configurations using continuous adjoint approach. 15th AIAA computational fluid dynamics conference. Restion: AIAA; 2001. p. AIAA2001-2580.

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