Aircraft Engineering
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
e-mail: s.parafes@mail.ru
Abstract
In paper a method of structural-parametric optimization of constructive-technological patterns of low-aspect lifting surfaces is proposed. The design structure is understood as the constructive-technological pattern. The choice of the best possible constructive-technological pattern is made as a result of the decision of an identification problem of alternative constructive-technological patterns with a preliminary found optimal design. The optimal design is a minimum of weight distribution of a material, satisfying with the requirement of strength and aeroelasticy. An example of structural-parametric optimization of constructive-technological patterns oj low-aspect lifting surfaces is given.
Keywords:
low-aspect lifting surfaces, aircraft, constructive-technological pattern, structural-parametric optimization, identification
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