Dynamic stability of unguided projectile with 6- DOF trajectory modeling
The paper presents the study of unguided rolling projectiles at varying Mach numbers using aerodynamic coefficients. The aerodynamic coefficients are estimated using an aerodynamic prediction code, Missile DATCOM. The predicted dynamic derivatives will determine the design criteria, and also their...
| Main Authors: | , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
IEEE Explorer
2017
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/1/08226280.pdf |