Wind-tunnel and Flight Investigations of the Use of Leading-edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 ̊swept-wing Airplane
Wind-tunnel and Flight Investigations of the Use of Leading-edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 ̊swept-wing AirplaneUnited States. National Advisory Committee for Aeronautics
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