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Featured researches published by Giorgio Cavallini.
Archive | 2012
Giorgio Cavallini; Roberta Lazzeri
Fatigue design of aerospace metallic components is carried out by using two methodologies: damage tolerance and safe-life. At present, regulations mainly recommend the use of the former, which entrusts safety to a suitable inspections plan. Indeed, a crack or a flaw is supposed to have been present in the component since the beginning of its operative life, and it must remain not critical, i.e. it must not cause a catastrophic failure in the life period between two following inspections, (Federal Aviation Administration, 1998; Joint Aviation Authorities, 1994; US Department of Defence, 1998). When a crack is detected, the component is repaired or substituted and the structural integrity is so restored.
20th ICAF Symposium, International Committee on Aeronautical Fatigue | 1999
Giorgio Cavallini; Roberto Galatolo; G. Cattaneo
19th ICAF Symposium (International Committee on Aeronautical Fatigue) | 1997
Giorgio Cavallini; Agostino Lanciotti; Luigi Lazzeri
24th Symposium of the International Committee on Aeronautical Fatigue | 2007
Giorgio Cavallini; Roberta Lazzeri
21th ICAF Symposium, International Committee on Aeronautical Fatigue | 2001
Giorgio Cavallini; Roberto Galatolo; Roberta Lazzeri
XV Congresso Nazionale dell'Associazione Italiana di Aeronautica | 1999
Giorgio Cavallini; Agostino Lanciotti; Luigi Lazzeri
Archive | 1999
Giorgio Cavallini; Roberto Galatolo
XIV Congresso Nazionale AIDAA, Associazione Italiana di Aeronautica e Astronautica | 1997
Giorgio Cavallini; Roberto Galatolo; Agostino Lanciotti; Luigi Lazzeri
Grandi Strutture in Lega Leggera saldate | 1994
Giorgio Cavallini; Roberto Galatolo; Agostino Lanciotti
4th Int. Conf. on fatigue and fatigue thresholds | 1990
Giorgio Cavallini; Agostino Lanciotti; Luigi Lazzeri
