Damage Tolerance Assessment of Bonded Composite Doubler Repairs for Commercial Aircraft Applications

Advances in the Bonded Composite Repair of Metallic Aircraft Structure

Volumn 1-2, Issue , 2002, Pages 485-516

  Roach, D ^a  

^a SANDIA NATIONAL LABORATORIES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; AIRCRAFT; CRACKS; DAMAGE DETECTION; LAMINATED COMPOSITES; SOFTWARE TESTING; STRAIN; STRUCTURAL PANELS;

COMMERCIAL AIRCRAFT; DAMAGE TOLERANCE ASSESSMENT; DELAMINATION FLAWS; DOUBLER TECHNOLOGY; ENVIRONMENTAL CONDITIONS; STRUCTURAL RESPONSE; TEMPERATURE AND HUMIDITIES; TOLERANCE CAPABILITY;

DAMAGE TOLERANCE;

EID: 84940849430     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-008042699-0/50019-X     Document Type: Chapter

References (26)

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