Research Article
Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay
Table 1
Mass attributes and ejection force parameters of the missile.
| | Mass, (kg) | 907.184 | | Center of mass, (m) | 1.417 | | Moment of inertia, (kg·m3) | 27.116 | | Moment of inertia, (kg·m3) | 488.094 | | The position of ejection force on the leading edge (m) | 1.2375 l | | The ejection force applied at the leading edge (N) | 10668.48 | | The position of ejection force on the trailing edge (m) | 1.7465 | | The ejection force applied at the trailing edge (N) | 42672.0 | | Operating distance (m) | 0.1 |
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