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- W2063878203 abstract "This paper reviews existing techniques for calculating dynamic loads for flexible airplanes and presents a new technique. The new technique involves the summation-of-forces method of writing dynamic loads equations. Until now, this form of the dynamic loads equations has been formulated in the frequency domain. The new technique uses 5-plane approximation methods (previously applied only to the equations of motion) to transform the dynamic loads equations from a second-order frequency domain formulation with frequency-dependent coefficients into a linear-lime-invariant state-space formulation. Several numerical examples demonstrate the usefulness of the new technique and the high quality of the results. In addition, a convergence investigation establishes that the summation-of-forces method converges more quickly (that is, with fewer modes) than does the mode displacement method." @default.
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- W2063878203 date "1986-04-01" @default.
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- W2063878203 title "New and existing techniques for dynamic loads analyses of flexible airplanes" @default.
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- W2063878203 doi "https://doi.org/10.2514/3.45309" @default.
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