Dynamic stability of unguided projectile with 6-
DOF trajectory modeling

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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...

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Bibliographic Details
Main Authors:	Bashir, Musavir, Khan, Sher Afghan, Udayagiri, Leelanadh, Noor, Asim
Format:	Proceeding Paper
Language:	English
Published:	IEEE Explorer 2017
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/1/08226280.pdf

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