【摘 要】
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The influences of airfoil thickness on the aerodynamic loading distribution and the hinge moments of folding wing aircraft are presented in this work. The tradi
【机 构】
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State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronau
论文部分内容阅读
The influences of airfoil thickness on the aerodynamic loading distribution and the hinge moments of folding wing aircraft are presented in this work. The traditional panel method shows deficiencies in the calculation of folding wing’s hinge moments. Thus, a thickness correction strat-egy for the aerodynamic model with CFD results is proposed, and an aeroelastic flight simulation platform is constructed based on the secondary development of ADAMS. Based on the platform, the developed aerodynamic model is verified, then the flight-folding process of the folding wing air-craft is simulated, and the influences of airfoil thickness on the results are investigated. Results show that the developed aerodynamic model can effectively describe the thickness effect of the folding wing. Airfoil thickness, which cannot be considered by the panel method, has a great influence on the hinge moments during the folding process, and the thickness correction has great significance in the calculation of folding wing’s hinge moments.
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