Natural Laminar Flow Optimization of Transonic Nacelle Based on Differential Evolution Algorithm-Reference-Cited by-同舟云学术

Natural Laminar Flow Optimization of Transonic Nacelle Based on Differential Evolution Algorithm

Published:2019-07 Issue:4 Volume:32 Page:06019001
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wang Shuyue¹^ORCID,Sun Gang²^ORCID,Li Chenghong³

Affiliation:

1. Ph.D. Candidate, Dept. of Aeronautics and Astronautics, Fudan Univ., 2617 Guanghua Tower(E), 220 Handan Rd., Shanghai 200433, China. ORCID: .

2. Professor, Dept. of Aeronautics and Astronautics, Fudan Univ., 2617 Guanghua Tower(E), 220 Handan Rd., Shanghai 200433, China (corresponding author). ORCID: .

3. Engineer, AECC Commercial Aircraft Engine Co., Ltd., 3998 Lianhua Rd.(S), Shanghai 200241, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001028

Reference35 articles.

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4. Aerodynamic Optimization of a Morphing Leading Edge Airfoil with a Constant Arc Length Parameterization

5. Carrigan T. J. 2011. “Aerodynamic shape optimization of a vertical axis wind turbine.” Ph.D. thesis Dept. of Aerospace Engineering Univ. of Texas at Arlington.

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