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- W2153603070 abstract "DOI: 10.2514/1.33445 An improved method is presented for estimating the subsonic location of the semispan aerodynamic center of a swept wing and the aerodynamic moment components about that aerodynamic center. The method applies to wings withconstantlineartaperandconstantquarter-chordsweep.Theresultsofacomputational fluiddynamicsstudyfor 236 wings show that the position of the semispan aerodynamic center of a wing depends primarily on aspect ratio, taperratio,andquarter-chordsweepangle.Wingaspectratiowasvariedfrom4.0to20,taperratiosfrom0.25to1.0 were investigated, quarter-chord sweep angles were varied from 0 to 50 deg, and linear geometric washout was variedfrom4:0to8:0 deg.AllwingshadairfoilsectionsfromtheNACA4-digitairfoilserieswithcambervaried from0to4%andthicknessrangingfrom6to18%.Withintherangeofparametersstudied,wingcamber,thickness, and twist were shown to have no significant effect on the position of the semispan aerodynamic center. The results of thisstudyprovideimprovedresolutionofthesemispanaerodynamiccenterandmomentcomponentsforconceptual design and analysis." @default.
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- W2153603070 date "2008-05-01" @default.
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- W2153603070 title "Estimating the Subsonic Aerodynamic Center and Moment Components for Swept Wings" @default.
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- W2153603070 doi "https://doi.org/10.2514/1.33445" @default.
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