Mathematical Problems in Engineering / 2013 / Article / Fig 5

Research Article

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

Figure 5

Variation of (a) flexural stiffness and (b) mass distribution, for a two-stage launch vehicle prior the launch [27].
764673.fig.005a
(a)
764673.fig.005b
(b)