Zobrazeno 1 - 10
of 26
pro vyhledávání: '"B-dul Iuliu Maniu"'
Autor:
Marius Gabriel Cojocaru, M. C. Fadgyas, Mihai Victor Pricop, Mihai Leonida Niculescu, M. G. Stoican, B-dul Iuliu Maniu, Dumitru Pepelea
Publikováno v:
INCAS Bulletin, Vol 8, Iss 3, Pp 55-64 (2016)
The temperature in the front region of a hypersonic vehicle nose can be extremely high, for example, reaching approximately 11 000 K at a Mach number of 36 (Apollo reentry) due to the bow shock wave. In this case, accurate prediction of temperature b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d4b07aa844e2a20e197172f45d3eb32c
https://doaj.org/article/af41c15ef5b740c4aa5f07f939e7fb06
https://doaj.org/article/af41c15ef5b740c4aa5f07f939e7fb06
Publikováno v:
INCAS Bulletin, Vol 8, Iss 2, Pp 109-122 (2016)
This paper is dedicated to the study and analysis of a successfully designed control system, whose capability should always maintain the stability and performance level in spite of the uncertainties in system dynamics and within the working environme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3d10b1e301e1d9c78dad3fb2d7934d27
http://bulletin.incas.ro/files/stroe__andrei__vol_8_iss_2__a_1.pdf
http://bulletin.incas.ro/files/stroe__andrei__vol_8_iss_2__a_1.pdf
Publikováno v:
INCAS Bulletin, Vol 7, Iss 1, Pp 13-28 (2015)
The main purpose of this paper is to develop some numerical experiences based on mechanical tests performed on MWCNT (Multi-wall carbon nanotubes) composites created in our Material compartment using finite element commercial codes (here NASTRAN). Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::526d58013e254c8360300b7c648db41a
https://doi.org/10.13111/2066-8201.2015.7.1.2
https://doi.org/10.13111/2066-8201.2015.7.1.2
Autor:
Emil Gabriel Costea, Minodor Arghir, B-dul Iuliu Maniu, Marina Andrei, Tiberiu Adrian Salaoru
Publikováno v:
INCAS Bulletin, Vol 6, Iss 4, Pp 115-123 (2014)
The method of Lamb waves to detect defects in aerospace structures is already known in research environments for its benefits, using an inexpensive equipment. The major benefits are: accurate determination of location and size of the defects in mater
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3f3809c619054ec175f70a991b886378
https://doi.org/10.13111/2066-8201.2014.6.4.11
https://doi.org/10.13111/2066-8201.2014.6.4.11
Publikováno v:
INCAS Bulletin, Vol 6, Iss 3, Pp 3-11 (2014)
The main goal of this paper is to present the implementation of an algorithm developed to calculate the Hurst exponent (H), applied here to characterize the pixel spectrum from hyperspectral image. Because a hyperspectral reflectance curve from each
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f4b52eb1429c9a8071a03defda451f83
https://doi.org/10.13111/2066-8201.2014.6.3.1
https://doi.org/10.13111/2066-8201.2014.6.3.1
Publikováno v:
INCAS Bulletin, Vol 6, Iss Special 1, Pp 3-13 (2014)
The basis for the aviation development is the ambition of increasing the efficiency and safety of flight. Improvements include flight performance and extended flight envelope, new flight regimes and tasks. However, all of these factors lead to the in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2ba7ad1a08c9b944c32a7673b3ab36a6
https://doi.org/10.13111/2066-8201.2014.6.s1.1
https://doi.org/10.13111/2066-8201.2014.6.s1.1
Autor:
Dorin Lozici-Brinzei, Radu Bisca, Elie Carafoli, Daniela Baran, Simion Tataru, B-dul Iuliu Maniu
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://explore.openaire.eu/search/publication?articleId=doi_dedup___::fec9bba55f09f2d456da57116a341500
https://doi.org/10.13111/2066-8201.2014.6.1.6
https://doi.org/10.13111/2066-8201.2014.6.1.6
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://explore.openaire.eu/search/publication?articleId=doi_dedup___::f604d5e8fa3d94af1fc69a416561c5c4
https://doi.org/10.13111/2066-8201.2013.5.3.1
https://doi.org/10.13111/2066-8201.2013.5.3.1
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://explore.openaire.eu/search/publication?articleId=doi_dedup___::3eedfdeb6351897f71dd35ebc9c625a7
http://bulletin.incas.ro/files/lozici_d__baran_d__tataru_s__v5_iss_2_full.pdf
http://bulletin.incas.ro/files/lozici_d__baran_d__tataru_s__v5_iss_2_full.pdf
Publikováno v:
INCAS Bulletin, Vol 5, Iss 1, Pp 87-93 (2013)
In this paper we are proposing a new approach in the numerical simulation of the blood flow in large vessels. The initial conditions are set to be compatible with the non-Newtonian model used. Numerical experiments in stenosed artery and in artery wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::84930649b9c55e8c76055a7dd2d16289
https://doi.org/10.13111/2066-8201.2013.5.1.9
https://doi.org/10.13111/2066-8201.2013.5.1.9