Status and development of laminar flow wing design technology

被引：0
|
作者：
Deng Y. [1 ]
Duan Z. [1 ]
Ai M. [1 ]
机构：
[1] Department of General and Aerodynamic Design, AVIC First Aircraft Institute, Xi'an
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2022年 / 43卷 / 11期
关键词：
drag reduction; flight test; green aviation; laminar wing; wind tunnel test;
D O I：
10.7527/S1000-6893.2021.26778
中图分类号：
学科分类号：
摘要：
The importance and necessity of aircraft drag reduction design are emphasized by analyzing the target of aircraft drag reduction proposed by green aviation, and the laminar wing technology is considered an important approach to aircraft drag reduction. After reviewing the development of laminar wing design, research, and verification, this paper identifies the gap and technical problems between the laminar wing technology and the aircraft design industry. The potential and development direction of the laminar wing technology are analyzed, and the feasibility of this technology in future aircraft design evaluated. © 2022 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
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