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- W566866092 abstract "Transonic wind tunnel tests have been performed to determine the twodimensional aerodynamic characteristics of a 16.5 % thick supercritical airfoil section. The section has been designed by NLR hodograph theory to be shock-free in potential flow at Moo= 0.721 and a lift coefficient of Ce= 0.595. The tests were conducted in the slotted test section of the NLR Pilot Tunnel at Mach numbers ranging from 0.2 to 0.825 and at angles of attack up to maximum lift. The Reynolds number based on the chord is about two million at the design condition. Lift, drag and pitching moment coefficients are presented and offdesign characteristics in terms of drag divergence, onset of rear separation, lift divergence and maximum lift are discussed." @default.
- W566866092 created "2016-06-24" @default.
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- W566866092 date "1976-05-24" @default.
- W566866092 modified "2023-09-27" @default.
- W566866092 title "Restricted aerodynamic characteristics of the supercritical shock-free airfoil section NLR 7201" @default.
- W566866092 hasPublicationYear "1976" @default.
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