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Nonlinear Time-Dependent Behaviour of Concrete Insulated Panel

2013

Abstract

"The insulated structural sandwich panel is a composite laminated structure, made of two stiff skin faces and lightweight thick core. The low-density low-shear rigidity laminated think core (foam, honeycomb) is structurally connected to the laminated skin faces by structural adhesive. The rigid skin (concrete, steel, wood) faces provide high bending stiffens for such lightweight structure, while the core resist the local buckling of the skin faces. The time-dependent deflection behaviour of the concrete insulated panel (CIP) varies with the change of the span-to-depth ratio for the instantaneous deflection, and the cyclic change of temperature and relative humidity over time. This paper discusses the nonlinear theoretical analysis for long-term creep deflection under sustained load that accounts for loads, time, temperature and relative humidity.

Key takeaways

  • Where; ∆ (t) = total time dependent deflection; ∆ o = initial deflection; A i = creep parameters associated with creep deflection equations; L: sustained load.
  • Where Δ o = instantaneous deflection (Δ o = σ/E), A 1 , A 2 , A 3 , A 4 = creep constants, L = applied load, T = temperature, θ = relative humidity, t = time, n = constant, and Δ f (t)= final deflection.
  • On the long-term of serviceability the fractional creep should be less than 4.0 at any time otherwise the sandwich beam will fail under flexural load.
  • ASTM C480-08, Standard Test Methods of Flexural Creep of Sandwich Construction (2008) covers the determination of the creep rate of sandwich panel under constant flexural load [22].
  • The total deflection accounts for the creep constant is multiplied by the long-term deflection and then summed to the instantaneous deflection.