Chandrasekhar's H-function

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File:Chandrasekhar's H-function.jpg
Chandrasekhar's H-function for different albedo

In atmospheric radiation, Chandrasekhar's H-function appears as the solutions of problems involving scattering, introduced by the Indian American astrophysicist Subrahmanyan Chandrasekhar.[1][2][3][4][5] The Chandrasekhar's H-function H(μ) defined in the interval 0μ1, satisfies the following nonlinear integral equation

H(μ)=1+μH(μ)01Ψ(μ)μ+μH(μ)dμ

where the characteristic function Ψ(μ) is an even polynomial in μ satisfying the following condition

01Ψ(μ)dμ12.

If the equality is satisfied in the above condition, it is called conservative case, otherwise non-conservative. Albedo is given by ωo=2Ψ(μ)=constant. An alternate form which would be more useful in calculating the H function numerically by iteration was derived by Chandrasekhar as,

1H(μ)=[1201Ψ(μ)dμ]1/2+01μΨ(μ)μ+μH(μ)dμ.

In conservative case, the above equation reduces to

1H(μ)=01μΨ(μ)μ+μH(μ)dμ.

Approximation

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The H function can be approximated up to an order n as

H(μ)=1μ1μni=1n(μ+μi)α(1+kαμ)

where μi are the zeros of Legendre polynomials P2n and kα are the positive, non vanishing roots of the associated characteristic equation

1=2j=1najΨ(μj)1k2μj2

where aj are the quadrature weights given by

aj=1P2n(μj)11P2n(μj)μμjdμj

Explicit solution in the complex plane

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In complex variable z the H equation is

H(z)=101zz+μH(μ)Ψ(μ)dμ,01|Ψ(μ)|dμ12,0δ|Ψ(μ)|dμ0, δ0

then for (z)>0, a unique solution is given by

lnH(z)=12πii+ilnT(w)zw2z2dw

where the imaginary part of the function T(z) can vanish if z2 is real i.e., z2=u+iv=u (v=0). Then we have

T(z)=1201Ψ(μ)dμ201μ2Ψ(μ)uμ2dμ

The above solution is unique and bounded in the interval 0z1 for conservative cases. In non-conservative cases, if the equation T(z)=0 admits the roots ±1/k, then there is a further solution given by

H1(z)=H(z)1+kz1kz

Properties

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  • 01H(μ)Ψ(μ)dμ=1[1201Ψ(μ)dμ]1/2. For conservative case, this reduces to 01Ψ(μ)dμ=12.
  • [1201Ψ(μ)dμ]1/201H(μ)Ψ(μ)μ2dμ+12[01H(μ)Ψ(μ)μdμ]2=01Ψ(μ)μ2dμ. For conservative case, this reduces to 01H(μ)Ψ(μ)μdμ=[201Ψ(μ)μ2dμ]1/2.
  • If the characteristic function is Ψ(μ)=a+bμ2, where a,b are two constants(have to satisfy a+b/31/2) and if αn=01H(μ)μndμ, n1 is the nth moment of the H function, then we have
α0=1+12(aα02+bα12)

and

(a+bμ2)01H(μ)μ+μdμ=H(μ)1μH(μ)b(α1μα0)

See also

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References

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  1. ^ Chandrasekhar, Subrahmanyan. Radiative transfer. Courier Corporation, 2013.
  2. ^ Howell, John R., M. Pinar Menguc, and Robert Siegel. Thermal radiation heat transfer. CRC press, 2010.
  3. ^ Modest, Michael F. Radiative heat transfer. Academic press, 2013.
  4. ^ Hottel, Hoyt Clarke, and Adel F. Sarofim. Radiative transfer. McGraw-Hill, 1967.
  5. ^ Sparrow, Ephraim M., and Robert D. Cess. "Radiation heat transfer." Series in Thermal and Fluids Engineering, New York: McGraw-Hill, 1978, Augmented ed. (1978).