NASA NACA-RM-L7I30-1947
Yaw characteristics and sidewash angles of a 42 degrees sweptback circular-arc wing with a fuselage and with leading-edge and split flaps at a Reynolds number of 5,300,000

Standard No.
NASA NACA-RM-L7I30-1947
Release Date
1947
Published By
National Aeronautics and Space Administration (NASA)



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