Abstract
The relative characteristics of motion of the fuel and shell upon launching is analyzed. By means of mechanical analysis and calculation, it is proposed that relative motion exists not only in the ranges between the fuel and shell of the warhead, but also in the fuel in different positions. The result of study indicates that the position of the fuel in the warhead has a marked influence on the relative motion, while the frictional coefficient between the fuel and shell has less influence upon it.
Original language | English |
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Pages (from-to) | 401-404 |
Number of pages | 4 |
Journal | Journal of Beijing Institute of Technology (English Edition) |
Volume | 11 |
Issue number | 4 |
Publication status | Published - Dec 2002 |
Keywords
- Angular velocity
- Fuel air explosive
- Launching
- Relative motion
- Warhead
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Yan, H., Zhang, Q., & Bai, C. H. (2002). Analysis on the motion characteristics of fuel and shell in launching. Journal of Beijing Institute of Technology (English Edition), 11(4), 401-404.