Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Stefan HOTHAZIE"'
Publikováno v:
INCAS Bulletin, Vol 11, Iss 1, Pp 61-77 (2019)
This paper presents the quasi-static thermo-mechanical loading effects on the progressive damage mechanisms and failure modes of the single-bolt, single-shear, hybrid metal-composite, bolted joints in aerospace applications. A three-dimensional finit
Externí odkaz:
https://doaj.org/article/122e5dc8d124411f8a019e1bd47d9521
Autor:
Stefan HOTHAZIE, Camelia-Elena MUNTEANU, Alexandra-Raluca PETRE, Ionut-Cosmin ONCESCU, Ion DIMA
Publikováno v:
INCAS Bulletin, Vol 10, Iss 4, Pp 71-84 (2018)
This paper presents an algorithm that calculates the nominal torque for friction grip joints, followed by its implementation in a Microsoft Excel worksheet that is automated by a macro written in Visual Basic. The algorithm outputs not only the optim
Externí odkaz:
https://doaj.org/article/bdd0b5fa93dd4823a2da765beabc264b
Publikováno v:
INCAS Bulletin, Vol 10, Iss 3, Pp 89-101 (2018)
Isogrid structures are a configuration of stiffeners of different sections, which make up a lattice placed on thin plates, with the aim of increasing the buckling factor of the overall structure. Because of the major benefits of isogrid structures wh
Externí odkaz:
https://doaj.org/article/aede4f71a326485bafd2a131c0f36e6d
Publikováno v:
INCAS Bulletin, Vol 10, Iss 2, Pp 207-220 (2018)
This paper presents a methodology for constructing iterative schemes of any order of convergence for solving nonlinear systems of equations. It also provides formulas for the order of convergence of any iterative schemes constructed using the method
Externí odkaz:
https://doaj.org/article/d7ae731017514bad896b632a452e8ac4
Autor:
Ion DIMA, Mihaela NASTASE, Stefan HOTHAZIE, Ionut-Cosmin ONCESCU, Camelia Elena MUNTEANU, Alexandru-Mihai CISMILIANU
Publikováno v:
INCAS Bulletin, Vol 9, Iss 4, Pp 59-74 (2017)
This article aims to provide an interactive in-house tool to quickly asses the stress in the critical points of the aeronautical structures. The software compares the results between the stress values obtained from the experimental tests using the re
Externí odkaz:
https://doaj.org/article/b7cd4561059e492a946ac0cff9a39614
Publikováno v:
INCAS Bulletin, Vol 11, Iss 1, Pp 61-77 (2019)
This paper presents the quasi-static thermo-mechanical loading effects on the progressive damage mechanisms and failure modes of the single-bolt, single-shear, hybrid metal-composite, bolted joints in aerospace applications. A three-dimensional finit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::06fb31812bc9293e514d1c213ad1343f
http://bulletin.incas.ro/files/coman__dima__hothazie__pelin__salaoru__vol_11_iss_.pdf
http://bulletin.incas.ro/files/coman__dima__hothazie__pelin__salaoru__vol_11_iss_.pdf