Obiekt

Współtwórca:

Sigitas KILIKEVIČIUS, Arvydas SURVILA, Laima PATAŠIENĖ ; Sigitas KILIKEVIČIUS, Arvydas SURVILA, Laima PATAŠIENĖ

Abstrakt:

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.
; 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.

Miejsce wydania:

Warszawa
; Warszawa

Wydawca:

Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna

Data utworzenia:

2010 r.0 ; 2010 r.0

Data złożenia:

2014-07-05 ; 2014-07-05

Data akceptacji:

2015-03-21 ; 2015-03-21

Data wydania:

2016-03-31 ; 2016-03-31

Rozmiar:

B5 ; B5

Identyfikator:

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

Sygnatura:

DOI 10.5604/20815891.1195197 ; DOI 10.5604/20815891.1195197

ISSN elektroniczny:

2720-5266 ; 2720-5266

ISSN drukowany:

2081-5891 ; 2081-5891

Język:

angielski ; angielski

Właściciel praw:

Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna

Strona początkowa:

7 ; 7

Strona końcowa:

16 ; 16

Tom:

7 ; 7

Słowa kluczowe:

aerodynamics, drag force, drag coefficient, rocket-target ; aerodynamics, drag force, drag coefficient, rocket-target