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NASA-CR-2779: Finite state modeling of aeroelastic systems
Abstract: A general theory of finite state modeling of aerodynamic loads on thin airfoils and lifting surfaces performing completely arbitrary, small, time-dependent motions in an airstream is developed and presented. The nature of ...
NASA-CR-2473: Effect of symmetrical vortex shedding on the longitudinal aerodynamic characteristics of wing-body-tail combinations
Abstract: An engineering prediction method for determining the longitudinal aerodynamic characteristics of wing-body-tail combinations is developed. The method includes the effects of nonlinear aerodynamics of components and the ...