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Nonlinear response of an aircraft to pulse excitation

โœ Scribed by G. Chandrasekharappa


Publisher
Elsevier Science
Year
1993
Tongue
English
Weight
361 KB
Volume
48
Category
Article
ISSN
0045-7949

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The response of a uniform clamped-free beam driven into the inelastic range by a half-sine pulse of ground acceleration is investigated. Shock spectra are presented for the case of bilinear moment-curvature relationships. The beam is represented as a ten-lump multi-degree-of-freedom system, and the