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...

Full description

Saved in:
Bibliographic Details
Main Authors: Bashir, Musavir, Khan, Sher Afghan, Udayagiri, Leelanadh, Noor, Asim
Format: Conference or Workshop Item
Language:English
Published: IEEE Explorer 2017
Subjects:
Online Access:http://irep.iium.edu.my/60787/1/08226280.pdf
http://irep.iium.edu.my/60787/
http://ieeexplore.ieee.org/document/8226280/
Tags: Add Tag
No Tags, Be the first to tag this record!
Be the first to leave a comment!
You must be logged in first