Experimental damping in pitch of 45 degree triangular wings

Murray Tobak, David E. Reese, Jr., Benjamin H. Beam
naca-rm-a50j26
Dec 1950


The results of an experimental wind-tunnel investigation of the damping in pitch of two triangular wings having leading edges swept back 45 degrees are presented. The wings differed only in airfoil section, one wing having a sharp leading-edge biconver section, the other a round leading edge section, NACA 0006-63.

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