Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Loris Molent"'
Autor:
Loris Molent, Russell Wanhill
Publikováno v:
Corrosion and Materials Degradation, Vol 2, Iss 3, Pp 493-511 (2021)
Corrosion-induced maintenance is a significant cost driver and availability degrader for aircraft structures. Although well-established analyses enable assessing the corrosion impact on structural integrity, this is not the case for fatigue nucleatio
Externí odkaz:
https://doaj.org/article/14b4b524555e48a8bc3e520b56e1712d
Autor:
Loris Molent
Publikováno v:
Materials Proceedings, Vol 6, Iss 1, p 23 (2021)
Metal fatigue management is generally well understood as reflected in the Aircraft Structural Integrity Management Plans, which, in some cases, consider environmental degradation prevention; however, limited provisions beyond find and fix exist for c
Externí odkaz:
https://doaj.org/article/699f89a52d1a489d88835d22f35d70ba
Publikováno v:
Journal of Aerospace Technology and Management, Vol 5, Iss 2 (2013)
http://dx.doi.org/10.5028/jatm.v5i2.219 The lead crack concept is adopted as the basis for a new fatigue lifing method using the safe life philosophy. As part of its management strategy, a full-scale fatigue test is conducted to identify high-risk lo
Externí odkaz:
https://doaj.org/article/b2e419725d0d46f6928c3a271fb43463
Autor:
Loris Molent, M.R. Fox
Maintaining aircraft airworthiness to ensure the fleet’s safe operation and maintain its readiness is critically dependent on accurate modelling and reliable predictions of fatigue crack growth. In this process a knowledge of the representative ini
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::01d3fbdecf8e46b9af19efe28e03a45b
https://doi.org/10.22541/au.167934195.53913189/v1
https://doi.org/10.22541/au.167934195.53913189/v1
Publikováno v:
International Journal of Fatigue. 102:214-220
Design of several metallic structural components, for instance in aerospace applications, should take into account the physically short crack behaviour. By characterising a fracture surface using fractals concepts, crack growth models similar to that
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9d030518edb432fcf62c023d953c2475
https://doi.org/10.1016/j.ijfatigue.2017.04.001
https://doi.org/10.1016/j.ijfatigue.2017.04.001
Publikováno v:
SpringerBriefs in Applied Sciences and Technology ISBN: 9789402416732
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::edaf8dc8388d455e4865d0f58072eb9a
https://doi.org/10.1007/978-94-024-1675-6
https://doi.org/10.1007/978-94-024-1675-6
Publikováno v:
SpringerBriefs in Applied Sciences and Technology ISBN: 9789402416732
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1c46ebabb0663d6b44c16731bf14751
https://doi.org/10.1007/978-94-024-1675-6_8
https://doi.org/10.1007/978-94-024-1675-6_8
Publikováno v:
SpringerBriefs in Applied Sciences and Technology ISBN: 9789402416732
In the mid-1980s Fokker Aircraft began a full-scale fatigue test of the fuselage and wings of the F100 aircraft [140]. During the test, which ran to 126,250 simulated flights, fatigue cracking occurred along one of the pressure cabin longitudinal lap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b648466544acfb1749c023f78598abe1
https://doi.org/10.1007/978-94-024-1675-6_9
https://doi.org/10.1007/978-94-024-1675-6_9
Publikováno v:
SpringerBriefs in Applied Sciences and Technology ISBN: 9789402416732
As discussed in Chap. 1, Sect. 1.2.4, the EBA is a framework for predicting the FCG lives of in-service aircraft structures subjected to relatively short and repeated blocks of VA loading sequences, i.e. load sequences representative for tactical air
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8bfd3b4c431459e613fc2de151d2948
https://doi.org/10.1007/978-94-024-1675-6_6
https://doi.org/10.1007/978-94-024-1675-6_6
Publikováno v:
SpringerBriefs in Applied Sciences and Technology ISBN: 9789402416732
In November1998 a Westland Lynx helicopter, operated by the Royal Netherlands Navy (RNLN), lost a rotor blade and then the rotor head just before take-off from the RNLN base at Den Helder, the Netherlands. Figure 11.1a shows the helicopter at an earl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7582d0165ac499478d26159bbeedb4d3
https://doi.org/10.1007/978-94-024-1675-6_11
https://doi.org/10.1007/978-94-024-1675-6_11