The wing, one of
the most important parts of aircraft, always requires sophis-ticated design to
increase lift, reduce drag and weight. For modern fixed-wing UAV, extending
cruising time is always a requirement for the overall design. Designing a most
light wing that can match the requirements of work condi-tions is desired. In
this work, according to the work conditions, we compare several types of wing
and chose beam-type wing. Then we made the detailed design and optimization to
reduce the weight of wing. At last, we draw the 3D model for potential
realistic production.
Raymer, D. (2012) Aircraft Design: A Conceptual Approach. 15th Edition.
https://doi.org/10.2514/4.869112
[4]
Hicks, R.M. and Henne, P.A. (1978) Wing Design by Numerical Optimization. Journal of Aircraft, 15, 407-412. https://doi.org/10.2514/3.58379
[5]
Young, J., Walker, S.M., Bomphrey, R.J., Taylor, G.K. and Thomas, A.L. (2009) Details of Insect Wing Design and Deformation Enhance Aerodynamic Function and Flight Efficiency. Science, 325, 1549-1552. https://doi.org/10.1126/science.1175928
[6]
Alexandrov, N., Lewis, R., Gumbert, C., Green, L. and Newman, P. (2000) Optimization with Variablefidelity Models Applied to Wing Design. 38th Aerospace Sciences Meeting and Exhibit, 841. https://doi.org/10.2514/6.2000-841
[7]
Vicini, A. and Quagliarella, D. (1999) Airfoil and Wing Design through Hybrid Optimization Strategies. AIAA Journal, 37, 634-641. https://doi.org/10.2514/2.764
[8]
NASA Wing Design Report, GRADES K-12.
[9]
Fang, Z.P. (2005) Aeronautical Aircraft Flight Dynamics. Beihang University Press.
[10]
Zhang, H.C. (2013) ANSYS 14.0 Theoretical Analysis and Engineering Application Examples. China Machine Press.
[11]
Liu, X.T. (2015) ANSYS Workbench Structural Engineering Advanced Application. China Water & Power Press.
[12]
Wang, X.M. (2007) ANSYS Numerical Analysis of Engineering Structure. China Communications Press.
