Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Simion Tataru"'
Publikováno v:
INCAS Bulletin, Vol 10, Iss 3, Pp 187-197 (2018)
The landing gear of an aircraft is an important part of the aircraft structure. The landing and the taking off are most critical parts of a flight mission. The main goal of this paper is to provide a methodology for designing and sizing the landing g
Externí odkaz:
https://doaj.org/article/552b3950b20f447d86b0be128643055c
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
Externí odkaz:
https://doaj.org/article/22709c66393e4755a6c347c8fe7e7aea
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
Externí odkaz:
https://doaj.org/article/75d0ae2672cb42e0a1ee52dfd10e689a
Publikováno v:
INCAS Bulletin, Vol 6, Iss 1, Pp 57-72 (2014)
The paper presents some methods of on-ground and in-flight calibration for strain gauges, intended to the development of complex programs which analyze the endurance phenomena for aerospace structures, with direct application to the IAR-99 Hawk. The
Externí odkaz:
https://doaj.org/article/00d5467d014d4234965272f88ad6f2d2
Publikováno v:
INCAS Bulletin, Vol 5, Iss 4, Pp 61-68 (2013)
This article aims to check the stress analysis technique based on 3D models also making a comparison with the traditional technique which utilizes a model built directly into the stress analysis program. This comparison of the two methods will be mad
Externí odkaz:
https://doaj.org/article/f511abcadf6449c2bbf4ce361a4ceeab
Publikováno v:
INCAS Bulletin, Vol 5, Iss 3, Pp 3-11 (2013)
This paper contains a dynamic study of the IAR-99 SOIM aircraft using ADAMS, multibody dynamic solutions. First, the analysis of the whole airplane is envisaged and then the analysis of the flight control system and the landing gear are considered. T
Externí odkaz:
https://doaj.org/article/0348717bc2a640e8992ceaefbdc80ad1
Publikováno v:
INCAS Bulletin, Vol 5, Iss 2, Pp 33-41 (2013)
Flutter analysis is considered for the minimum altitude at which the minimum designed Mach number is achieved, for the maximum altitude at which the maximum designed dynamic pressure is obtained and for the minimum altitude at which transonic effects
Externí odkaz:
https://doaj.org/article/39294ae408e24b528241de9df7777f97
Publikováno v:
INCAS Bulletin, Vol 4, Iss 3, Pp 31-40 (2012)
The hundreds of parameters that are recorded by Flight Data Recorders (FDR) during flight facilitates the investigation of incidents and also provides the opportunity to use the recorded data to predict future aircraft behaviour.Current researches ar
Externí odkaz:
https://doaj.org/article/fa10ed5c842642a09428f30b3e7fe357
Publikováno v:
INCAS Bulletin, Vol 4, Iss 2, Pp 157-167 (2012)
As a general rule the final step in every aviation program is the certification of the airplane, an important step in which the airplane, the engins and the equipments are checked by an authority or commission according to the airworthiness rules. Th
Externí odkaz:
https://doaj.org/article/5072643fb58846cfa020a5dc1f6ed887
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
Externí odkaz:
https://doaj.org/article/9569b54c9bae418b9abe2e74e9b0d7a0