NASA NACA-TN-1417-1947
High-speed wind-tunnel tests of an NACA 0009-64 airfoil having a 33.4-percent-chord flap with an overhang 20.1 percent of the flap chord

Standard No.

NASA NACA-TN-1417-1947

Release Date

1947

Published By

National Aeronautics and Space Administration (NASA)