NASA NACA-TN-2819-1952
Effect of high-lift devices on the static-lateral-stability derivatives of a 45 degree sweptback wing of aspect ratio 4.0 and taper ratio 0.6 in combination with a body

Standard No.

NASA NACA-TN-2819-1952

Release Date

1952

Published By

National Aeronautics and Space Administration (NASA)