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Interval-based optimization of aircraft wings under landing loads
Authors:Luna Majumder  SS Rao
Affiliation:Department of Mechanical and Aerospace Engineering, University of Miami, Coral Gables, Miami, FL 33124-0624, United States
Abstract:An interval-based automated optimization of aircraft wing structures subjected to landing loads is discussed in this paper. The interaction between landing gear and flexible airplane structure is considered as a coupled system. The uncertain system parameters are described as interval numbers. The computational aspects of the optimization procedure are illustrated with two examples – symmetric double-wedge airfoil, and supersonic airplane wing. Since, in most cases only the ranges of uncertain parameters are known with their probability distribution functions unknown, the present methodology is expected to be more realistic for the optimum design of aircraft structures under landing loads.
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