Zobrazeno 1 - 10
of 37
pro vyhledávání: '"A.N. Chamos"'
Publikováno v:
International Journal of Structural Integrity. 11:861-873
PurposeThe purpose of this paper is to investigate the fatigue behavior of precipitation-strengthened Cu‒2.55Ni‒0.55Si alloy, modified by the addition of 0.25 Cr and 0.25 Zr (wt%), using mechanical and fractographical studies to reveal the effect
Autor:
Bernd Mayer, A.N. Chamos, Pawel Malinowski, A.G. Stamopoulos, Michael Noeske, Kai Brune, Hauke Brüning, Welchy Leite Cavalcanti, Romain Ecault, Thomas Krousarlis, Konstantinos Tserpes, Wieslaw Ostachowicz
Publikováno v:
Adhesive Bonding of Aircraft Composite Structures ISBN: 9783319928098
The first chapter highlights the relevance of both adhesive bonding technology and in-process quality assessment for mastering twenty-first-century challenges in joining functional and lightweight materials like carbon fibre reinforced polymers. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a3ab2263afa8cc374af581bf66583f12
https://doi.org/10.1007/978-3-319-92810-4_1
https://doi.org/10.1007/978-3-319-92810-4_1
Autor:
Konstantinos Tserpes, Welchy Leite Cavalcanti, Andreas Helwig, Kai Brune, Romain Ecault, Célian Cherrier, Johannes Derksen, Saverio De Vito, Laurent Berthe, Mareike Schlag, Tomasz Wandowski, Wieslaw Ostachowicz, Damien Segur, Pawel Malinowski, Hauke Brüning, Rainer Stössel, Ana Reguero Simon, Maxime Sagnard, Mirosław Sawczak, A.N. Chamos
Publikováno v:
Adhesive Bonding of Aircraft Composite Structures ISBN: 9783319928098
This chapter highlights two advances towards a higher maturity of versatile extended non-destructive testing (ENDT) procedures. Full-scale demonstration tests are presented in realistic user application cases that involve typical production or repair
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b1032830e9e3701c5a91d2c4cda4a57
https://doi.org/10.1007/978-3-319-92810-4_5
https://doi.org/10.1007/978-3-319-92810-4_5
Publikováno v:
Frattura ed Integrità Strutturale, Vol 11, Iss 42, Pp 9-22 (2017)
Frattura ed Integrità Strutturale, Vol 11, Iss 42 (2017)
Frattura ed Integrità Strutturale; Vol. 11 No. 42 (2017): October 2017; Pages 9-22
Frattura ed Integrità Strutturale; V. 11 N. 42 (2017): October 2017; Pages 9-22
Frattura ed Integrità Strutturale, Vol 11, Iss 42 (2017)
Frattura ed Integrità Strutturale; Vol. 11 No. 42 (2017): October 2017; Pages 9-22
Frattura ed Integrità Strutturale; V. 11 N. 42 (2017): October 2017; Pages 9-22
In a series of applications, steel reinforced concrete structures are subjected to fatigue loads during their service life, what in most cases happens in corrosive environments. Surface treatments have been proved to represent proper processes in ord
Publikováno v:
Fatigue & Fracture of Engineering Materials & Structures. 40:1551-1561
Publikováno v:
Theoretical and Applied Fracture Mechanics. 83:60-66
In this study, the fatigue behavior of Cu–2.55Ni–055Si alloy specimens was investigated by fractographical analysis. Fatigue specimens were prepared according to ISO 1099 standard and constant amplitude loading was applied at a stress ratio (R =
Publikováno v:
International Journal of Structural Integrity. 7:25-46
Purpose – The purpose of this paper is to quantify the corrosion damage evolution that has occurred on the aircraft aluminum alloy 2024 after the exposure to Exfoliation Corrosion Test (EXCO) solution. Moreover, the effect of the evolving corrosion
Publikováno v:
MATEC Web of Conferences, Vol 188, p 02011 (2018)
The precipitation hardenable and non-toxic Cu-Ni-Si alloys are good alternatives to Cu-Be and Cu-Co-Ni-Be alloys due to their high strength and high conductivity that can be attained by not only alloying but also thermo-mechanical routes. In this stu
Publikováno v:
Journal of Materials Engineering and Performance. 22:2253-2260
The formability of Titanium alloy sheet material Ti-40 has been experimentally assessed in the present investigation. The investigation is divided into two parts: In the first part, the effect of the strain rate applied during testing, as well as the
Publikováno v:
Theoretical and Applied Fracture Mechanics. 58:55-64
A concept for tolerating corrosion damage on aircraft aluminum structures is outlined. The proposed concept is based on experimental observations. Observed has been that local cladding patterns are sufficient to keep reductions of both, tensile and f