November 2018
Intermediate to advanced
768 pages
24h 4m
English
| A | Transverse inertia moment of the projectile, cross‐section area, linearization coefficient |
| Matrix of system, rotation matrix | |
| a | Acceleration of the mass center of the projectile |
| ap | Axial acceleration of original point o0 of rocket launcher coordinate system ooxoyozo relative to the launching guider |
| Bz, |
Linearization coefficients |
| C | Polar inertia moment of the projectile, mass center of the rigid body, linearization coefficient |
| C j | Damping coefficient of damper j |
| Damping coefficient of torsional damper j | |
| Damping matrix | |
| D | Action point of exterior forces, interphase drag |
| D1, D3 | Operator |
| Dx , Dy, Dxy | Bending stiffness of the plate |
| dp | Equivalent diameter of the propellant grain |
| Dp | Diameter of the propellant grain |
| Dz , |
Linearization coefficients |
| d1, d3 | Operator |
| d0 | Rotating band diameter of the projectile |
| E | Young’s modulus |
| Transform matrix | |
| EA | Tensile stiffness |
| EI | Bending stiffness of the beam |
| EX |