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Fatigue and Fracture of Engineering Materials and Structures

Volumn 25, Issue 2, 2002, Pages 151-172

Shape optimization of critical stiffener runouts for F-111 airframe life extension

(4) Heller, M a,b Mcdonald, M a Burchill, M a Watters, K C a

a AERO AND MAR RESEARCH LABORATORY (Australia)

b DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION (Australia)

Author keywords

Finite element procedure; Gradient less method; Life extension; Shape optimization; Stress concentrators

Indexed keywords

FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; FRACTURE TOUGHNESS; GRADIENT METHODS; LOAD TESTING; RESIDUAL STRESSES; STRESS CONCENTRATION; TENSILE STRESS; WINGS;

COLD PROOF LOAD TESTING; CRITICAL STIFFENER RUNOUTS; FUEL FLOW VENT HOLES; SHAPE OPTIMIZATION; WING PIVOT FITTING;

AIRFRAMES;

EID: 0036466229 PISSN: 8756758X EISSN: None Source Type: Journal
DOI: 10.1046/j.8756-758x.2001.00.x Document Type: Article

Times cited : (8)

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