Stability Criteria of Projectile During Flight in Varying Density Atmosphere

Authors

  • T. N. Srivastava Defence Science Laboratory, Delhi

DOI:

https://doi.org/10.14429/dsj.16.7241

Keywords:

Aerodynamic forces, Atmosphere, Projectile

Abstract

Stability of the projectile in a varying density atmosphere is investigated under general set up of aerodynamic forces and torques. For circular trajectories, necessary and sufficient stability criteria are developed. Relationship between stability and optimality is outlined. The results have been illustrated by numerical examples.

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Published

2014-05-15

How to Cite

Srivastava, T. N. (2014). Stability Criteria of Projectile During Flight in Varying Density Atmosphere. Defence Science Journal, 16(3), 137–144. https://doi.org/10.14429/dsj.16.7241

Issue

Vol. 16 No. 3

Section

Research Papers

License

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