Analytical solution to approximate equations of the launch vehicle motion under the gust action for the dynamic loading calculation
Introduction. The launch vehicle (LV) in flight and the dynamic components of loads from the impact of a trapezoidal wind gust are considered. It is proposed to determine the dynamic components of the force factors using analytical solutions for the structure points accelerations. The work objective...
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| Format: | Article |
| Language: | Russian |
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Don State Technical University
2022-03-01
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| Series: | Advanced Engineering Research |
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| Online Access: | https://www.vestnik-donstu.ru/jour/article/view/1832 |