王彬文1, 杨宇1, 钱战森2, 王志刚1, 吕帅帅1, 孙侠生3
CJA
收稿日期:2020-11-02
修回日期:2020-12-15
出版日期:2022-01-15
发布日期:2020-12-14
通讯作者:
杨宇
E-mail:18313341@qq.com
WANG Binwen1, YANG Yu1, QIAN Zhansen2, WANG Zhigang1, LYU Shuaishuai1, SUN Xiasheng3
Received:2020-11-02
Revised:2020-12-15
Online:2022-01-15
Published:2020-12-14
摘要： 通过改变机体结构气动外形，确保飞行器在不同飞行状态下持续获得最优气动效益，一直是航空领域的研究热点，而机翼变弯度（VCW）技术是其中一个重要研究方向。首先，分析总结了机翼变弯度技术所带来的综合收益，详细阐述了不同飞行器对机翼变弯度技术的具体需求；然后，分别从变弯度前缘和后缘回顾了过去数十年的发展历程，分析了当前面临的主要技术难点；最后，预测了未来发展趋势，并对机翼变弯度技术的未来研究方向提出了建议。
中图分类号:
王彬文, 杨宇, 钱战森, 王志刚, 吕帅帅, 孙侠生. 机翼变弯度技术研究进展[J]. 航空学报, 2022, 43(1): 24943-024943.
WANG Binwen, YANG Yu, QIAN Zhansen, WANG Zhigang, LYU Shuaishuai, SUN Xiasheng. Technical development of variable camber wing: Review[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 24943-024943.
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