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- W2378383422 abstract "An optimal design configuration of leading edge extensions(LEXs) is presented based on the standard genetic algorithms(GAs).Aircraft longitudinal dynamic response of the system with and without LEX is analyzed by solving the state equation of aircraft longitudinal motion.Aerodynamic force,moments,and longitudinal stability derivatives are estimated by three-dimensional low-order panel method.A novel aircraft model with LEX is optimized and its lift curve slope is increased by 13%—17% for Ma=0.4—0.9 and 12% for Ma=1.5.Numerical results show that because the frequency and damping ratio in a short period are improved,the aircraft rapidly responds to a specified deflection control input in the battle area when LEX is installed.Finally,compared the results from the panel method with those from the Cy-20 aircraft flight test data,aerodynamic characteristics are verified." @default.
- W2378383422 created "2016-06-24" @default.
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- W2378383422 date "2007-01-01" @default.
- W2378383422 modified "2023-09-25" @default.
- W2378383422 title "AIRCRAFT LIFT AND LONGITUDINAL RESPONSE ENHANCEMENT BY OPTIMIZATION OF LEADING EDGE EXTENSION CONFIGURATION" @default.
- W2378383422 hasPublicationYear "2007" @default.
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