Feasibility study on damage tolerance design of titanium alloys

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 30, Issue 4, 2009, Pages 763-767

  Zhang, Jikui ^a   Li, Zhengneng ^a   Qiu, Zhiping ^a   Lei, Jiafeng ^b   Li, Hongen ^c   Yu, Yang ^d  

^a BEIHANG UNIVERSITY   (China)

^b INSTITUTE OF METAL RESEARCH   (China)

^c SHENYANG AIRCRAFT DESIGN AND RESEARCH INSTITUTE   (China)

^d GENERAL RESEARCH INSTITUTE FOR NONFERROUS METALS   (China)

Author keywords

Crack growth; Damage tolerance; Extra low interstitial; Structural design; Titanium alloys; Total fatigue life

Indexed keywords

AIRCRAFT STRUCTURES; CRACK GROWTH; CRACK GROWTH LIVES; CRACK PROPAGATION RATES; DAMAGE TOLERANCE METHODS; EQUIVALENT LOADINGS; EXTRA-LOW INTERSTITIAL; FEASIBILITY STUDIES; METAL MATERIALS; RESIDUAL STRENGTHS; STRUCTURE DESIGNS; TOTAL FATIGUE LIFE;

AIRCRAFT; AIRCRAFT MANUFACTURE; AIRCRAFT MATERIALS; AIRFRAMES; ALUMINA; ALUMINUM ALLOYS; ARCHITECTURAL DESIGN; CERIUM ALLOYS; CRACK PROPAGATION; CRACKING (CHEMICAL); CRACKS; DAMAGE TOLERANCE; DECISION MAKING; FATIGUE DAMAGE; FITS AND TOLERANCES; FRACTURE; FRACTURE TOUGHNESS; IMPLANTS (SURGICAL); MATERIALS PROPERTIES; PLANNING; RECONSTRUCTION (STRUCTURAL); RESOURCE ALLOCATION; STRUCTURAL DESIGN; TITANIUM;

TITANIUM ALLOYS;

EID: 65549113562     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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