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Wind-tunnel investigation of the effects of flap span and deflection angle, wing platform and a body on the high-lift performance of a 28° swept wing

Wind-tunnel investigation of the effects of flap span and deflection angle, wing platform and a body on the high-lift performance of a 28° swept wing - - London Her Majesty's Stationary Office 1976 - 198 p. - ARC CP 1372 : 1976 .

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Universal Decimal Class. No.: DARC CP 1372 : 1976

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