An investigation was made in the Ames Aeronautical Laboratory 7- by 10-foot wind tunnel of the effects of various modifications to the profile of a 0.20-chord plain sealed aileron on an NACA 66,2-216 (a = 0.6) airfoil.
An investigation was made in the Ames Aeronautical Laboratory 7- by 10-foot wind tunnel of the effects of a trailing edge of a 0.20-chord plain sealed aileron on an NACA 66,2-216 (a = 0.6) airfoil.
- A. M. Peiser, Abbott A. Putnam, Clinton E. Brown, Eugene E. Lunquist, Macon C. Ellis, Robert M. Crane, Robert T. Jones, Sidney J. Shames, Wilbur L. Mayo, William A. Benser, United States. National Advisory Committee for Aeronautics, Elbridge Z. Stowell, Hermon M. Parker, Jason J. Moses, M. Wilkerson, Ralph W. Holtzclaw, Evan H. Schuette
· 1944
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