NASA NTRS · 19710000187
Peak structural response to nonstationary random excitations
Abstract
Study establishes distribution function of peak response values, based on frequency interpretation. Excitations considered include impact loading on landing gears and aircraft gust loading. Because of relative severity of excitations, prediction of fatigue and maximum response characteristics is important part of task of structural analysis and design.
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Shinozuka, M., Yang, J.-N.. 1971-06-01. Peak structural response to nonstationary random excitations. https://ntrs.nasa.gov/citations/19710000187
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