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- W274214354 abstract "Abstract : A circulation control uncambered elliptic airfoil section with a thickness-to-chord ratio of 0.20 was tested subsonically to determine its aerodynamic characteristics. Lift coefficients up to 5 were produced at momentum coefficients, of 0.24. The initially high unblown drag coefficients, characteristic of bluff trailing edge airfoils, were greatly reduced at low values of momentum coefficient. It was therefore possible to produce equivalent lift-to-drag ratios in excess of 30 when Cl = 1.0. The ability to produce high lift coefficients essentially independent of angle of attack is indicated by the results of this investigation." @default.
- W274214354 created "2016-06-24" @default.
- W274214354 creator A5081696674 @default.
- W274214354 date "1975-06-01" @default.
- W274214354 modified "2023-09-25" @default.
- W274214354 title "Two-Dimensional Subsonic Wind Tunnel Evaluation of a 20-Percent-Thick Circulation Control Airfoil" @default.
- W274214354 doi "https://doi.org/10.21236/ada027164" @default.
- W274214354 hasPublicationYear "1975" @default.
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