Measurements of the dynamic response of the Rosman I 85-foot dish antenna
Natural vibration frequencies, modal damping factors, transfer functions, and source of tracking errors for Rosman I 85-foot dish antenna
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Natural vibration frequencies, modal damping factors, transfer functions, and source of tracking errors for Rosman I 85-foot dish antenna
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Computerized simulation of control systems for nuclear light bulb engine during start-up and at nominal full power operation
A semi-analytical method is developed for the calculation of the response of nonuniform structures to deterministic and random excitation. The method is based on parametric representations of the impulse response and input functions. With these representations, a class of structures of specified geometry and a class of pressure fields of practical concern can be considered simultaneously in a single analytical calculation of structural response. In engineering applications, the parameters in the impulse response function can be fixed once the numerical solution of the associated eigenvalue problem is available; the input function parameters can be specified given a particular input function or pressure field data. This methodology is applied to nonuniform beams and circular cylindrical shells for which parametric response solutions are derived. The computerized version of these solutions is also presented.