Fatigue crack growth in patched plates under constant amplitude and flight simulation loadings
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Fatigue crack growth in patched plates under constant amplitude and flight simulation loadings
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| Creator |
Chandra, R
Sunder, R |
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| Subject |
Structural Mechanics
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| Description |
Fatigue crack propagation was studied in aluminium alloy
plates reinforced by adhesive bonding a unidirectional carbon
fibre epoxy patch across the crack path. The tests were
carried out under constant amplitude as well as flight
simulation combat aircraft spectrum loading. Comparative
tests were also conducted on unpatched plates. The composite
patch considerably reduces crack growth rates. The improvement
in resistance to fatigue crack growth is more pronounced under
spectrum loading conditions.
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| Type |
Conference or Workshop Item
PeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/11850/1/fatigue.pdf
Chandra, R and Sunder, R Fatigue crack growth in patched plates under constant amplitude and flight simulation loadings. In: 6th International Conference on Fracture (ICF6)., 4-10 Dec 1984, New Delhi. |
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| Relation |
http://nal-ir.nal.res.in/11850/
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