The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 and 45 degrees of sweepback at Mach numbers to 0.92 /

Main Authors: Demele, Fred A.
Corporate Authors: United States. National Advisory Committee for Aeronautics.
Group Author: Powell, K. Harmon.
Published:
Call Number: V224/D376