Mathematical Problems in Engineering / 2013 / Article / Tab 3

Research Article

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

Table 3

A comparison of TMM using different numbers of segments with flight test and computed data.

TMM Flight test [27]
time from launch
(0.25 to 0.75 sec)
Computed data [27]
time from launch
(0.0 to 1.0 sec)
ModeNumber of segments
501004001000

112.9537.1810.5810.58 10.510.5 to 10.9
211.5535.7535.0335.02
310.5866.2562.4162.54