Effect of Airfoil Dimple on Low-Reynolds-Number Differing Laminar Separation Behavior via Multi-Objective Optimization-Reference-Cited by-同舟云学术

Effect of Airfoil Dimple on Low-Reynolds-Number Differing Laminar Separation Behavior via Multi-Objective Optimization

Published:2022-09 Issue:5 Volume:59 Page:1243-1256
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Liang Yu¹^ORCID,Yang Yannian¹,Shan Xiaowen¹^ORCID,Wang Zican¹

Affiliation:

1. Southern University of Science and Technology, 518055 Shenzhen, People’s Republic of China

Funder

National Science Foundation of China

Southern Marine Science and Engineering Guangdong Laboratory

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036558

Reference36 articles.

1. GasterM. “The Structure and Behaviour of Laminar Separation Bubbles,” AGARD CP-4, 1966, pp. 813–854. 10.1.1.226.9783

2. HortonH. P. “Laminar Separation Bubbles in Two and Three Dimensional Incompressible Flow,” Doctoral Dissertation, Queen Mary Univ. of London, London, 1968.

3. McgheeJ. R.WalkerB. S.MillardB. F. “Experimental Results for the Eppler387 Airfoil at Low Reynolds Numbers in the Langley Low-Turbulence Pressure Tunnel,” NASA TM 4062, 1988.

4. The influence of laminar separation and transition on low Reynolds number airfoil hysteresis

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