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.

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http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-l51d25.pdf