Zobrazeno 1 - 10
of 22
pro vyhledávání: '"TATARU, Simion"'
Publikováno v:
In Procedia Engineering 2014 69:1430-1436
Autor:
BARAN, Daniela1 baran.daniela@incas.ro, TATARU, Simion2 tataru.simion@incas.ro, PETRE, Mihaela2 petre.mihaela@incas.ro
Publikováno v:
INCAS Bulletin. 2018, Vol. 10 Issue 3, p187-197. 11p.
Publikováno v:
INCAS Bulletin, Vol 9, Iss 2, Pp 159-173 (2017)
This paper presents a methodology for identifying some stress concentrators based on the modal analysis performed using MSC Patran and MSC Nastran programs. The influence of a beam crack on its own frequency is practically insignificant. In order to
Publikováno v:
INCAS Bulletin, Vol 9, Iss 1, Pp 125-138 (2017)
This article presents a selection of parameters recorded within the No. 719 IAR-99 HAWK flights and processed through the original software developed by the authors in Excel language. Flights were made at CCÎZ Craiova. The results processing leads t
Publikováno v:
Proceedings of the Scientific Conference AFASES. May2011, p1129-1134. 27p.
Autor:
LOZICI-BRINZEI, Dorin1 lozicid@incas.ro, TATARU, Simion2 sitataru@incas.ro, BISCA, Radu1 biscar@incas.ro, BARAN, Daniela1 dbaran@incas.ro
Publikováno v:
INCAS Bulletin. 2014, Vol. 6 Issue 1, p57-72. 16p.
Publikováno v:
INCAS Bulletin, Vol 4, Iss 1, Pp 125-132 (2012)
The program IAR 99 SOIM was start in 1991 as an integral Romanian program for aviation in witch the specialists from Institutul National de Cercetare-Dezvoltare Aerospatiala "Elie Carafoli" INCAS developed a trainer aircraft realized at the best aero
Publikováno v:
INCAS Bulletin, Vol 3, Iss 3, Pp 151-156 (2011)
In this presentation, we will concentrate on the vertical support, which is free from all sides. A Finite Element Model (FEM) of the IAR-93 aircraft monument has been developed in PATRAN/NASTRAN®, partly from a previous ANSYS® model FEM can be used
Publikováno v:
INCAS Bulletin, Vol 1, Iss 2, Pp 129-135 (2009)
In the aerospace industry one of the most important requirements in the aircraft design and operation is the high level of fiability under various atmosphere and environmental conditions. The design and validation of such a system is a great challeng
Autor:
Tataru Simion, Apostolescu Nicolae, Caloian Bogdan, Lozici Dorin, Baran Daniela, Bisca Radu, Stere Marcel
Publikováno v:
INCAS Bulletin, Vol 1, Iss 1, Pp 93-95 (2009)
The main objective of this project is to develop a set of tools and to integrate techniques in a software package which is build on structure analysis applications based on Romanian engineers experience in designing and analysing aerospace structures