Composite repairs to rib stiffened panels

There are several methods available for obtaining a first estimate for the design of composite repairs to cracks in thin metallic skins. One approach uses analytical formulae, which build on an analogy with the problem of a bonded symmetric lap joint (Rose LRF. An application of the inclusion analog...

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Veröffentlicht in:	Composite structures 1999-12, Vol.47 (1), p.737-743
Hauptverfasser:	Ting, T., Jones, R., Chiu, W.K., Marshall, I.H., Greer, J.M.
Format:	Artikel
Sprache:	eng
Schlagworte:	Bonded repair Boron patches Composite solids Composites Condensed matter: structure, mechanical and thermal properties Cross-disciplinary physics: materials science rheology Deformation and plasticity (including yield, ductility, and superplasticity) Exact sciences and technology Fatigue, brittleness, fracture, and cracks Fracture Material form Mechanical and acoustical properties of condensed matter Mechanical properties of solids Physics Rheology Stiffened wing skins
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