Some effects of fuselage interference, wing interference, and sweepback on the damping in roll of untapered wings as determined by techniques employing rocket-propelled vehicles

William M. Bland, Jr., Albert E. Dietz
naca-rm-l51d25
Oct 1951


An experimental investigation employing techniques which utilized rocket-propelled vehicles in free flight has been made to determine some effects of fuselage interference, wing interference, and sweepback on the damping-in-roll characteristics of untapered wings with an aspect ratio of 3.7 and NACA 65A009 airfoil sections between Mach number 0.6 and Mach number 1.7.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-l51d25.pdf