Research Article

Transfer Matrix Method for the Determination of the Natural Vibration Characteristics of Realistic Thrusting Launch Vehicle—Part I

Figure 7

Effects of shear deformation and rotary inertia on (a) mode shape, (b) rotation angle, (c) moment, and (d) shear of first mode for : ♦ Timoshenko model; —Euler-Bernoulli model.
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(a)
764673.fig.007b
(b)
764673.fig.007c
(c)
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(d)