Calculative method for estimating the interference pressure field at zero lift on a symmetrical swept-back wing mounted on a circular cylindrical body

Jack N. Nielsen, Frederick H. Matteson
naca-rm-a9e19
Aug 1949


An approximate method is presented for calculating the interference pressure distribution at zero lift of a symmetrical swept-back wing mounted on a circular cylindrical body with the chord plane of the wing passing through the axis of the body.

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