language-icon Old Web
English
Sign In

Heisler chart

Heisler charts are a graphical analysis tool for the evaluation of heat transfer in thermal engineering. They are a set of two charts per included geometry introduced in 1947 by M. P. Heisler which were supplemented by a third chart per geometry in 1961 by H. Gröber. Heisler charts permit evaluation of the central temperature for transient heat conduction through an infinitely long plane wall of thickness 2L, an infinitely long cylinder of radius ro, and a sphere of radius ro. Heisler charts are a graphical analysis tool for the evaluation of heat transfer in thermal engineering. They are a set of two charts per included geometry introduced in 1947 by M. P. Heisler which were supplemented by a third chart per geometry in 1961 by H. Gröber. Heisler charts permit evaluation of the central temperature for transient heat conduction through an infinitely long plane wall of thickness 2L, an infinitely long cylinder of radius ro, and a sphere of radius ro. Although Heisler-Gröber charts are a faster and simpler alternative to the exact solutions of these problems, there are some limitations. First, the body must be at uniform temperature initially. Additionally, the temperature of the surroundings and the convective heat transfer coefficient must remain constant and uniform. Also, there must be no heat generation from the body itself. These first Heisler-Gröber charts were based upon the first term of the exact Fourier Series solution for an infinite plane wall: T ( x , t ) − T ∞ T i − T ∞ = ∑ n = 0 ∞ [ 4 sin ⁡ λ n 2 λ n + sin ⁡ 2 λ n e − λ n 2 α t L 2 cos ⁡ λ n x L ] {displaystyle {frac {T(x,t)-T_{infty }}{T_{i}-T_{infty }}}=sum _{n=0}^{infty }{left}} , where Ti is the initial temperature of the slab, T∞ is the constant temperature imposed at the boundary, x is the location in the plane wall, λn is π(n+1/2), and α is thermal diffusivity. The position x=0 represents the center of the slab. The first chart for the plane wall is plotted using 3 different variables. Plotted along the vertical axis of the chart is dimensionless temperature at the midplane, θo* = T ( 0 , t ) − T ∞ T i − T ∞ {displaystyle ={frac {T(0,t)-T_{infty }}{T_{i}-T_{infty }}}} . Plotted along the horizontal axis is the Fourier Number, Fo=αt/L2 . The curves within the graph are a selection of values for the inverse of the Biot Number, where 'Bi = hL/k. k is the thermal conductivity of the material and h is the heat transfer coefficient.' The second chart is used to determine the variation of temperature within the plane wall for different Biot Numbers. The vertical axis is the ratio of a given temperature to that at the centerline θ/θo = T ( x , t ) − T ∞ T ( 0 , t ) − T ∞ {displaystyle ={frac {T(x,t)-T_{infty }}{T(0,t)-T_{infty }}}} where the x/L curve is the position at which T is taken. The horizontal axis is the value of Bi−1.

[ "Convection", "Heat transfer", "Cylinder (engine)", "Biot number", "Thermal conduction" ]
Parent Topic
Child Topic
    No Parent Topic