Aerodynamic optimization of a high-lift system with adaptive dropped hinge flap

被引：8

作者：

Ji, Qiang ^{[1
,2
]}

Zhang, Yufei ^{[1
]}

Chen, Haixin ^{[1
]}

Ye, Junke ^{[3
]}

机构：

[1] Tsinghua Univ, Sch Aerosp Engn, Beijing 100084, Peoples R China

[2] 63870 PLA Troops, Huayin 714200, Peoples R China

[3] Shanghai Aircraft Design & Res Inst, Shanghai 200236, Peoples R China

来源：

CHINESE JOURNAL OF AERONAUTICS | 2022年 / 35卷 / 11期

基金：

中国国家自然科学基金;

关键词：

Adaptive dropped hinge flap; Aerodynamic design; High-Lift aerodynamics; Multidisciplinary optimiza-tion; Optimization of aircraft design; DOWNWARD DEFLECTION; DESIGN; STRATEGIES;

D O I：

10.1016/j.cja.2022.03.012

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The Adaptive Dropped Hinge Flap (ADHF) is a novel trailing edge high-lift device char-acterized by the integration of downward deflection spoiler and simple hinge flap, with excellent aerodynamic and mechanism performance. In this paper, aerodynamic optimization design of an ADHF high-lift system is conducted considering the mechanism performance. Shape and settings of both takeoff and landing configurations are optimized and analyzed, with considering the kine-matic constraints of ADHF mechanism, and the desired optimization results were obtained after optimization. Sensitivity analysis proves the robustness of the optimal design. Comparison shows that the ADHF design has better comprehensive performance of both mechanism and aerodynam-ics than the conventional Fowler flap and simple hinge flap design.(c) 2022 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

引用

页码：191 / 208

页数：18