The effects of Reynolds number at Mach numbers up to 0.94 on the loading on a 35 degree swept-back wing having NACA 65(1)A012 streamwise sections

Bruce E. Tinling, Armando E. Lopez
naca-rm-a52b20
Jun 1952


An investigation has been made of the effects of a variation of Reynolds number on the forces, moments, and surface pressures on a semispan model of a wing having 35 degrees of sweepback, an aspect ratio of 5, a taper ratio of 0.7, and the NACA 65(1)A012 section in planes parallel to the plane of symmetry.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-a52b20.pdf