An affordable methodology for replacing metallic aircraft panels with advanced composites

Composites - Part A: Applied Science and Manufacturing

Volumn 33, Issue 5, 2002, Pages 687-696

  Baker, A A ^a   Callus, P J ^a   Georgiadis, S ^b   Falzon, P J ^c   Dutton, S E ^c   Leong, K H ^c  

^a AERO AND MAR RESEARCH LABORATORY   (Australia)

^b HdH Boeing   (Australia)

^c Cooperative Research Centre for Advanced Composite Structures Ltd ^*  (Australia)

Author keywords

A. Prepreg; B. Damage tolerance; D. Mechanical testing; E. Tooling

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; HONEYCOMB STRUCTURES; MECHANICAL TESTING; STRUCTURAL PANELS;

ADVANCED COMPOSITES;

COMPOSITE MATERIALS;

EID: 0036567252     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1359-835X(02)00013-1     Document Type: Article

References (9)

1. Repair substantiation fatigue testing including temperature and frequency effects for a bonded composite repair to an F-111 lower wing skin
2. Certification basis for a demonstrator composite replacement panel
3. Fatigue damage in composite laminates
4. Bonded composite repair of fatigue-cracked primary aircraft structure