Molent et al., 1993 - Google Patents
Crack growth and repair of multi-site damage of fuselage lap jointsMolent et al., 1993
- Document ID
- 9438193315057524928
- Author
- Molent L
- Jones R
- Publication year
- Publication venue
- Engineering fracture mechanics
External Links
Snippet
A fatigue test program was conducted to investigate multi-site damage of commerical wide- bodied aircraft fuselage lap joints. Crack growth data were generated using specimens representative of a typical lap joint. It was also demonstrated that a boron/epoxy composite …
- 210000001503 Joints 0 title abstract description 17
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
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