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
naca-rm-a9b16
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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1949/naca-rm-a9b16.pdf