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- W2367097304 abstract "According to the technical requirements of autonomous flight,the aircraft's aerodynamic loads on the experimental design of the layout are studied In the low Reynolds number,through wind tunnel tests designed miniature streak wing aircraft for aerodynamic performance evaluation, obtained aerodynamic parameters.Drag coefficient for wind-tunnel measurements of the defects is too large,and the low Reynolds number,wind tunnel data on the inaccuracy in absolute value. Previous experience of using the existing formula and innovative approach to the wind tunnel data processing,use small angle of attack range of parameters that are relatively reasonable,the results of the empirical formula and the correction.Be more reasonable control of identification parameters in order to achieve autonomous flight of small aircraft." @default.
- W2367097304 created "2016-06-24" @default.
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- W2367097304 date "2010-01-01" @default.
- W2367097304 modified "2023-09-23" @default.
- W2367097304 title "A Small Trim-wing Unmanned Aircraft Aerodynamic Parameter Estimation and Analysis of Wind Tunnel Test" @default.
- W2367097304 hasPublicationYear "2010" @default.
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