机翼变弯度技术研究进展

doi:10.7527/S1000-6893.2020.24943

Abstract

Abstract: The Variable Camber Wing(VCW) remains a research hot-spot as it aims to ensure that aircraft acquire optimal aerodynamic efficiency in various flight conditions. The benefits brought by VCWs are firstly presented, and the demands of VCWs from different types of aircraft are classified and thoroughly described. The developing process of VCWs in the past decades are then reviewed in terms of the leading edge and the trailing edge, respectively, and the current major obstacles in application are listed. Further research directions are finally suggested.

Key words: morphing structure, variable camber wing(VCW), compliant structure, leading edge, trailing edge

CLC Number:

V214.19

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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Technical development of variable camber wing: Review

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