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FEA Course Lecture V

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FEA Course Lecture V Outline UCSD - 10/30/03 Review of Last Lecture (IV) on Plate and Shell Elements. Thermal Analysis Summary of Concepts of Heat Transfer – PowerPoint PPT presentation

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Title: FEA Course Lecture V


1
  • FEA Course Lecture V Outline
  • UCSD - 10/30/03
  • Review of Last Lecture (IV) on Plate and Shell
    Elements.
  • Thermal Analysis
  • Summary of Concepts of Heat Transfer
  • Thermal Loads and Boundary Conditions
  • Nonlinear Effects
  • Thermal transients and Modeling Considerations
  • Example FE

2
  • Thermal Analysis - Introduction
  • Thermal Analysis involves calculating
  • Temperature distributions
  • Amount of Heat lost or gained
  • Thermal gradients
  • Thermal fluxes.
  • There are two types of thermal analysis
  • Steady-state analysis
  • Transient thermal analysis

3
  • Two types of Thermal Analysis
  • Steady-state Thermal Analysis. It involves
    determining the temperature distribution and
    other thermal quantities under steady-state
    loading conditions. A steady-state loading
    condition is a situation where heat storage
    effects varying over a period of time can be
    ignored.
  • Some examples of thermal loads are
  • Convections
  • Radiation
  • Heat Flow Rates
  • Heat Fluxes (Heat Flow/unit area)
  • Heat Generation Rates (heat flow/unit volume)
  • Constant Temperature Boundaries
  • Steady State thermal analysis may be linear or
    nonlinear (due to material properties not
    geometry). Radiation is a nonlinear problem.
  • Transient Thermal Analysis. It involves
    determining the temperature distribution and
    other thermal quantities under conditions that
    vary over a period of time.

4
Theoretical Basis for Thermal Analysis
  • KT T Q where KT f
    (conductivity of material).
  • T vector of nodal temperatures
  • Q vector of thermal loads.
  • KT is nonlinear when radiation heat transfer is
    present. Note that convection and radiation BCs
    contribute terms to both KT and Q.
  • Heat is transferred to or from a body by
    convection and radiation.

Heat Flow across boundary due to radiation
(in-out)
Prescribed rate of heat flow across boundary (in
or out)
Heat generated internally (eg., Joule heating)
Prescribed temperature (BC) insulated for
example.
Heat Flow across boundary due to radiation
(in-out)
5
Equation of Heat Flow (1D Systems)
  • fx -k dT/dx Fourier Heat Conduction
    Equation. Heat flows from high
  • temperature region to low temperature region.
  • Q -kA dT/dx Q heat flow
  • fx Q/A where fx heat flux/unit area, k
    thermal conductivity, A area of cross-section,
    dT/dx temperature gradient
  • In general, fx, fy, fz -kdT/dX, dT/dY,
    dT/dZ T
  • For an elemental area of length dx, the balance
    of energy is given as
  • -KA dT/dx qAdx rca dT/dt dx KA dT/dx
    d/dx(KA dT/dx)dx
  • d/dx(KA dT/dx) Aq rca dT/dt
  • rate in rate out rate of increase within
  • For generally anisotropic material
  • -d/dx d/dy d/dz fx fy fzT qv cr
    dT/dt
  • where c is specific heat, t is time, r mass
    density and qv rate of internal heat generation
    / unit volume.
  • Above equation can be re-written as
  • Steady state if dT/dt 0

6
Some Notes
  • If the body is plane and there is convection and
    or radiation heat transfer across its flat
    lateral surfaces, additional equations for flux
    terms are needed
  • Convection BC
  • f h(Tf T) (Newtons Law of cooling)
  • K f(h)
  • Q f(h,Tf)
  • where f flux normal to the surface Tf
    temperature of surrounding fluid h heat
    transfer coefficients (which may depend on many
    factors like velocity of fluid,
    roughness/geometry of surface, etc) and T-
    temperature of surface.
  • Radiation BC
  • f hr(Tr T)
  • K f(hr)
  • Q f(hr,T)
  • where, Tr temperature of the surface hr
    temperature dependent heat transfer coefficients.
  • hr Fs(Tr2T2)(TrT).
  • Where F is a factor that accounts for geometries
    of radiating surfaces.s is Stefan-Boltzmann
    constant.

7
FEs in Thermal Analysis
  • 1D Bar Element
  • Uniform bar whose lateral surface is insulated
  • 2D Elements
  • PLANE35, PLANE55, PLANE77 etc.
  • 3D Elements
  • SOLID70, SOLID90 etc.
  • Transient Thermal Analysis
  • KTT CT Q where Q Q(t)
  • T dT/dt,
  • C Summation of c
  • Solution Use Crank Nicholson Method, etc.
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