Wind-tunnel investigation of a tailless triangular-wing fighter aircraft at Mach numbers from 0.5 to 1.5

Leslie F. Lawrence, James L. Summers
Jun 1949

A wind-tunnel investigation has been made to determine the respective variations with Mach number of the static longitudinal stability, the drag, and the effectiveness of a constant-chord control surface for a tailless fighter aircraft employing a triangular wing of aspect ratio 2.31.

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