Search U.S. government technical reports digitized or harvested by TRAIL.
Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range
Flutter of a 60©� delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model
Supersonic flutter of a 60©� delta wing encountered during the flight test of a rocket-propelled model
Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model
Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6
Flutter at very high speeds