Application of flaw tolerance methodologies to rotorcraft fatigue qualification

31st European Rotorcraft Forum

Volumn 2005, Issue , 2005, Pages

  Mariani, U ^a   Vicario, M ^a  

^a LEONARDO S P A   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTRIC LOADS; FATIGUE OF MATERIALS; HELICOPTERS; ROTORS; STRUCTURAL ANALYSIS; SYSTEMS ANALYSIS;

CATASTROPHIC FAILURE; ROTORCRAFT FATIGUE TOLERANCE; SAFE-LIFE METHODOLOGIES; TAIL ROTOR COMPONENTS;

FAULT TOLERANT COMPUTER SYSTEMS;

EID: 33746632182     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. FAR 29 Airworthiness Standards: Transport Category Rotorcraft /JAR 29 Large Rotorcraft
2. th September, Marseilles, France
3. S. Beretta, M. Giglio, U. Mariani, M. Vicario, Flaw Tolerance Evaluation of Helicopter Rotor Part, ICAF 2003, Lucern, Switzerland
4. Murakami, Y., Metal Fatigue: Effects of Small Defects and Non metallic Inclusion, Elsevier, UK, 2002
5. th of small cracks emanating from small defects In: The Behaviour of Short Fatigue Cracks, Edited by K.J. Miller and E.R. de Los Rios, MEP, London, 1986.
6. Murakami, Y., Effects of small defects and inhomogeneities on fatigue strength: experiments, model and application to industry. ECF-11 Mechanisms and Mechanics of Damage and Failure, pp. 31-42, Petit, J. (Ed.), EMAS, Warley, 1996.
7. AFGROW - USAF Crack growth prediction program
8. AC 20-107A - Composite Aircraft Structure