Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 2 with NACA 0005-63 section

Donald W. Smith, John C. Heitmeyer
naca-rm-a50k21
Feb 1951


A wing-body combination having a plane triangular wing of aspect ratio 2 and NACA 0005-63 sections in streamwise planes has been investigated at both subsonic and supersonic Mach numbers. The lift, drag, and pitching moment of the model are presented for Mach numbers from 0.24 to 0.95 and from 1.30 to 1.70 at a Reynolds number of 3.0 million.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-a50k21.pdf