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- W174602020 abstract "Oscillatory aerodynamic lift and pitching moment derivatives have been measured in a wind tunnel at low subsonic speeds on the following wing and wing-body combinations:(i) tapered wing of aspect ratio 1.3, mid-chord line unswept, with a sharp leading edge,(ii) above wing fitted with a nacelle in three chordwise positions at the tip,(iii) wing at (i) fitted with a tip body representing a tank or store, and tested with and without a fin at the rear of the body.The measured derivatives for the wing alone are in good agreement with values calculated using lifting surface theory, and are in reasonable agreement with values calculated using a semi-empirical methode.Derivatives for the wing with nacelle in the central position have been calculated using a semi-empirical method which makes an allowance for aerodynamic interference effects, and comparison shows that the values are reasonably accurate." @default.
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- W174602020 date "1963-03-31" @default.
- W174602020 modified "2023-09-28" @default.
- W174602020 title "Measurements of aerodynamic derivatives on a wing with a series of tip bodies" @default.
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