=+7. Repeat the same dynamic response analysis under antisymmetric loading (Figure 5.31). Note: All results can be
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=+7. Repeat the same dynamic response analysis under antisymmetric loading (Figure 5.31).
Note: All results can be obtained in nondimensional form by assuming that the beam characteristics (bending stiffness EI, mass per unit length m, wing half-span and load intensity p0 have unit value).
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Mechanical Vibrations Theory And Application To Structural Dynamics
ISBN: 9781118900208
3rd Edition
Authors: Michel Geradin, Daniel J. Rixen
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