Mathematical Problems in Engineering / 2013 / Article / Fig 6

Research Article

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

Figure 6

Parameters of a multistage launch vehicle [5]: (a) flexural stiffness, (b) shear rigidity, (c) mass, and (d) radius of gyration.
764673.fig.006a
(a)
764673.fig.006b
(b)
764673.fig.006c
(c)
764673.fig.006d
(d)