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Journal of Aerospace Engineering

Volumn 14, Issue 4, 2001, Pages 140-146

Reliability analysis of rotorcraft composite structures

(5) Mahadevan, S a Dey, A a Tryon, R a Wang, Y a Rousseau, C a

a VANDERBILT UNIVERSITY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); COMPOSITE STRUCTURES; CRACKS; DELAMINATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; HELICOPTER ROTORS; LAMINATED COMPOSITES; MATERIALS TESTING; MATHEMATICAL MODELS; PROBABILITY; RELIABILITY;

COMPOSITE HELICOPTER ROTOR HUB TEST; COMPOSITE LAMINATE ANALYSIS; FATIGUE FAILURE MODELING; FATIGUE LOADING; FATIGUE RELIABILITY; RELIABILITY ANALYSIS; ROTORCRAFT COMPOSITE STRUCTURES;

AEROSPACE ENGINEERING;

EID: 0035482868 PISSN: 08931321 EISSN: None Source Type: Journal
DOI: 10.1061/(ASCE)0893-1321(2001)14:4(140) Document Type: Article

Times cited : (19)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.