Effect of Thrust on the Structural Vibrations of a Nonuniform Slender Rocket
The vibration characteristics of a nonuniform, flexible and free-flying slender rocket experiencing constant thrust is investigated. The rocket is idealized as a classic nonuniform beam with a constant one-dimensional follower force and with free-free boundary conditions. The equations of motion are...
| Published in: | Mathematical and Computational Applications |
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| Main Authors: | , , |
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2020-05-01
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| Subjects: | |
| Online Access: | https://www.mdpi.com/2297-8747/25/2/29 |