Transonic Axial-Flow Blade Shape Optimization Using Evolutionary Algorithm and Three-Dimensional Navier-Stoke Solver

Author:

Oyama Akira,Liou Meng-Sing,Obayashi Shigeru

Publisher

American Institute of Aeronautics and Astronautics

Cited by 23 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Optimization of transonic low-Reynolds number airfoil based on genetic algorithm;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-11-14

2. Design Optimization of 1.5-Stage Transonic Compressor Based on BPNN Surrogate Model and NSGA-II;Machines;2023-06-06

3. Coupling Genetic Algorithm with an Artificial Neural Network for Optimization of a Supercritical CO2 Compressor;AIAA SCITECH 2023 Forum;2023-01-19

4. CFD—A Powerful Visualization Tool in Turbomachinery Applications;Lecture Notes in Mechanical Engineering;2019-09-28

5. Multidisciplinary Design and Optimizations of Swept and Leaned Transonic Rotor;Journal of Engineering for Gas Turbines and Power;2017-08-23

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