Výsledky vyhledávání - "Laima PATAŠIENĖ"

Akademický článek

Design, Research and Practical Implementation of the Laser Shooting Simulation System for 5.56 mm G-36, 7.62 mm FN MAG and 84 mm carl Gustaf

Autor: Algimantas FEDARAVIČIUS, Arvydas SURVILA, Laima PATAŠIENĖ, Egidijus SLIŽYS

Publikováno v: Problemy Mechatroniki, Vol 7, Iss 2, Pp 7-18 (2016)

Riflemen’s trainers are efficiently applied for the training of the armed forces, police, and shooting sportsmen. However, the training quality directly depends on the perfection of trainers as well as on their functional facilities. One of them is

Externí odkaz: https://doaj.org/article/96fb7ca724a1488cb9a9a40958855193

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Akademický článek

Analysis of Aerodynamic Characteristics of the Rocket-Target for the „Stinger' System

Autor: Algimantas FEDARAVIČIUS, Sigitas KILIKEVIČIUS, Arvydas SURVILA, Laima PATAŠIENĖ

Publikováno v: Problemy Mechatroniki, Vol 7, Iss 1, Pp 7-16 (2016)

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 comput

Externí odkaz: https://doaj.org/article/199315c54d2d49f685429267cbf36822

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Design, Research and Practical Implementation of the Laser Shooting Simulation System for 5.56 mm G-36, 7.62 mm FN MAG and 84 mm carl Gustaf

Autor: Egidijus Sližys, Laima Patašienė, Algimantas Fedaravičius, Arvydas Survila

Publikováno v: Problemy Mechatroniki, Vol 7, Iss 2, Pp 7-18 (2016)

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::69dc00ee632dfc73532c02c39d8f2973
http://publisherspanel.com/gicid/pdf/01.3001.0008.5741

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Design of the testing system for solid propellant rocket motor thrust measurements using mathematical modelling techniques

Autor: Algimantas Fedaravičius, Saulius Račkauskas, Arvydas Survila, Laima Patašienė

Publikováno v: Journal of Measurements in Engineering, Vol 3, Iss 4, Pp 123-131 (2015)

This paper describes design technique of solid fuel rocket motor testing system for its thrust measuring capabilities. The design process consists of 2 parts. In first part the mathematic modelling technique will be described for the mechanical secti

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doajarticles::0fabb4a633ef396d84cab71ac91b8208
https://www.jvejournals.com/article/16760

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