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- W2391759098 abstract "Towards the requirement of medium-altitude long-endurance( MALE) unmanned aerial vehicle( UAV),the required high-lift,low-torque laminar airfoil was designed. Airfoil was parameterized by the class function /shape function method,aerodynamic solution used XFOIL software,and multi-objective genetic algorithm NSGA-II was selected for optimization. The performance of designed airfoil was checked by N-S equation based on transition model. Calculation results show that optimized airfoil has obvious fore-loading characteristics,high cruising lift-to-drag ratio,small nose-down moment,and has the ability of not causing flight safety problem due to earlier transition. Optimized airfoil has well met the design requirements,and has good engineering practicability." @default.
- W2391759098 created "2016-06-24" @default.
- W2391759098 creator A5052939566 @default.
- W2391759098 date "2014-01-01" @default.
- W2391759098 modified "2023-09-25" @default.
- W2391759098 title "Integrated design of high-lift laminar airfoil for MALE UAV" @default.
- W2391759098 hasPublicationYear "2014" @default.
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