Aerodynamic Shape Optimization of Natural-Laminar-Flow Wing Using Surrogate-Based Approach-Reference-Cited by-同舟云学术

Aerodynamic Shape Optimization of Natural-Laminar-Flow Wing Using Surrogate-Based Approach

Published:2018-07 Issue:7 Volume:56 Page:2579-2593
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Han Zhong-Hua¹,Chen Jing¹,Zhang Ke-Shi¹,Xu Zhen-Ming¹,Zhu Zhen¹,Song Wen-Ping¹

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

Funder

Aeronautical Science Foundation of China

ATCFD Project

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056661

Reference53 articles.

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2. VikenJ. K.Watson-VikenS. A.PfenningerW.MorganH. L. Jr.CampbellR. L. “Design of the Low-Speed NLF (1)-0414F and the High-Speed HSNLF (1)-0213 Airfoils with High-Lift Systems,” NASA CP-2487, 1987, pp. 637–671.

3. SomersD. M. “Design and Experimental Results for a Natural-Laminar-Flow Airfoil for General Aviation Applications,” NASA TP-1865, 1981.

4. A Class of Airfoils Designed for High Lift in Incompressible Flow

5. KhalidM.JonesD. J. “A Summary of Transonic Natural Laminar Flow Airfoil Development at NAE,” Rept. NAE AN-65, National Research Council Canada, Ottawa, ON, 1990.

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