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Ohman, L.H. (author), Dixon, R.C. (author)
Flutter analysis of a rocket fin at Mach numbers from 2 to 7 has been performed. The analysis is based on a number of preassigned mode shapes with piston theory representing the aerodynamic forces. Various mode combinations, effects of reduced stiffness due to kinetic heating, effects of structural damping and thickness effects as given by 2nd...
report 1963