Mathematical Problems in Engineering / 2013 / Article / Fig 9

Research Article

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

Figure 9

Effects of shear deformation and rotary inertia on the first three natural vibrations on moment ((a), (b), (c)) and shear force ((d), (e), (f)) for upper stage of the launch vehicle ( ): - - - Timoshenko model; —Euler-Bernoulli model.