Object

Contributor:

Sigitas KILIKEVIČIUS, Arvydas SURVILA, Laima PATAŠIENĖ

Abstract:

This paper presents an analysis of aerodynamic characteristics of the rocket-target for the final training of shooting at aerial targets by the „Stinger” system service staff. The governing equations of fluid dynamics are presented and the computational model of airflow around the rocket is developed. ANSYS CFX computational fluid dynamics software is used to compute airflow velocities, pressure, the drag force and the drag coefficient. A practical implementation of the research is presented. Taking into account the simulation results, the rocket-target was designed and manufactured.

Place of publishing:

Warszawa

Publisher:

Wojskowa Akademia Techniczna

Date created:

2010 r.0

Date submitted:

2014-07-05

Date accepted:

2015-03-21

Date issued:

2016-03-31

Extent:

B5

Identifier:

oai:ribes-88.man.poznan.pl:2268

Call number:

DOI 10.5604/20815891.1195197

Electronic ISSN:

2720-5266

Print ISSN:

2081-5891

Language:

angielski

Rights holder:

Wojskowa Akademia Techniczna

Starting page:

7

Ending page:

16

Volume:

7

Keywords:

aerodynamics, drag force, drag coefficient, rocket-target