Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade

Designing the high-performance, high-subsonic airfoils suitable for different Reynolds number flow is the major challenge for high-altitude long-endurance drones and ultra-high altitude solar aircraft. To overcome the difficulties, this paper proposed a set of aerodynamic optimization design methods...

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Bibliographic Details

Published in:	Engineering Applications of Computational Fluid Mechanics
Main Authors:	Song Huang, Xingen Lu, Ge Han, Shengfeng Zhao, Chuangxin Zhou, Chengwu Yang
Format:	Article
Language:	English
Published:	Taylor & Francis Group 2022-12-01
Subjects:	optimization design high-subsonic airfoil improved whale optimization algorithm boundary layer displacement thickness reynolds number
Online Access:	http://dx.doi.org/10.1080/19942060.2021.2020170