Analysis and optimization of a camber morphing wing model

Author:

Li Bing12,Li Gang12

Affiliation:

1. State Key Laboratory of Robotics and System (HIT), Harbin, P.R. China

2. Shenzhen Graduate School, Harbin Institute of Technology, Shenzhen, P. R. China

Abstract

This article proposes a camber morphing wing model that can continuously change its camber. A mathematical model is proposed and a kinematic simulation is performed to verify the wing’s ability to change camber. An aerodynamic model is used to test its aerodynamic characteristics. Some important aerodynamic analyses are performed. A comparative analysis is conducted to explore the relationships between aerodynamic parameters, the rotation angle of the trailing edge, and the angle of attack. An improved artificial fish swarm optimization algorithm is proposed, referred to as the weighted adaptive artificial fish-swarm with embedded Hooke–Jeeves search method. Some comparison tests are used to test the performance of the improved optimization algorithm. Finally, the proposed optimization algorithm is used to optimize the proposed camber morphing wing model.

Publisher

SAGE Publications

Subject

Artificial Intelligence,Computer Science Applications,Software

Reference43 articles.

1. Obradovic B. Modeling and simulation of the flight dynamics of morphing wing aircraft. Thesis, University of Texas, Arlington, 2010.

2. Supekar AH. Design, analysis and development of a morphable wing structure for unmanned aerial vehicle performance augmentation. Thesis. University of Texas, Arlington, 2007.

3. Realization of an optimized wing camber by using formvariable flap structures

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