Attaining flaw-tolerant design life objectives in helicopter rotor system lugs

30th European Rotorcraft Forum

Volumn 2005, Issue , 2005, Pages 471-480

  Mariani, U ^a   Ratti, G ^a   Reid, L ^b  

^a Fatigue Department   (Italy)

^b Fatigue Technology Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; BUSHINGS; CRACK INITIATION; DATABASE SYSTEMS; DEFECTS; FATIGUE TESTING; FITS AND TOLERANCES; TITANIUM ALLOYS;

AGUSTAWESTLAND COMPANY (CO); BUSHING INSTALLATION METHODS; FATIGUE TECHNOLOGY INC. (CO); FLAW TOLERANCE;

HELICOPTER ROTORS;

EID: 33745572399     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (0)