201931st International Symposium on BallisticsRequires access

An Innovative Stabilizer Unit Design for Tube Launched Artillery Rocket to Improve Dynamic Stability

Nitika Mittal, A. Anandaraj, K. M. RAJAN

Open publisher page 0 citations

Abstract

In this paper, stabilizer unit of the tube launched artillery rocket is designed with flat wrap around fins (WAF). A comparative study has been carried out to find out the aerodynamic behavior of same rocket with curved and flat WAF. Computational fluid dynamic (CFD) is used to find out aerodynamic coefficients of the rocket with both types of fins. It is found that with flat WAF chances of occurrence of out-of-plane moment reduced drastically. Hence, it is recommended to use Flat WAF for tube launch rocket to avoid any

About this research paper

What this paper is about

In this paper, stabilizer unit of the tube launched artillery rocket is designed with flat wrap around fins (WAF). A comparative study has been carried out to find out the aerodynamic behavior of same rocket with curved and flat WAF. Computational fluid dynamic (CFD) is used to find out aerodynamic coefficients of the rocket with both types of fins. It is found that with flat WAF chances of occurrence of out-of-plane moment reduced drastically. Hence, it is recommended to use Flat WAF for tube launch rocket to avoid any

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

In this paper, stabilizer unit of the tube launched artillery rocket is designed with flat wrap around fins (WAF). A comparative study has been carried out to find out the aerodynamic behavior of same rocket with curved and flat WAF. Computational fluid dynamic (CFD) is used to find out aerodynamic coefficients of the rocket with both types of fins. It is found that with flat WAF chances of occurrence of out-of-plane moment reduced drastically. Hence, it is recommended to use Flat WAF for tube launch rocket to avoid any

Key concepts: Rocket (weapon), Artillery, Aerospace engineering, Stabilizer (aeronautics), Launched, Tube (container), Aerodynamics, Engineering

Related papers

Back to paper searchBrowse research topicsOriginal source
An Innovative Stabilizer Unit Design for Tube Launched Artillery Rocket to Improve Dynamic Stability — Research Paper | ScholarLens