Physics:Chandrasekhar's H-function

From HandWiki
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 0≤μ≤1, satisfies the following nonlinear integral equation

H(μ)=1+μH(μ)∫01Ψ(μ′)μ+μ′H(μ′)dμ′

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

∫01Ψ(μ)dμ≤12.

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)=[1−2∫01Ψ(μ)dμ]1/2+∫01μ′Ψ(μ′)μ+μ′H(μ′)dμ′.

In conservative case, the above equation reduces to

1H(μ)=∫01μ′Ψ(μ′)μ+μ′H(μ′)dμ′.

Approximation

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

H(μ)=1μ1⋯μn∏i=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=2∑j=1najΨ(μj)1−k2μj2

where aj are the quadrature weights given by

aj=1P2′n(μj)∫−11P2n(μj)μ−μjdμj

Explicit solution in the complex plane

In complex variable z the H equation is

H(z)=1−∫01zz+μH(μ)Ψ(μ)dμ,∫01|Ψ(μ)|dμ≤12,∫0δ|Ψ(μ)|dμ→0, δ→0

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

ln⁡H(z)=12πi∫−i∞+i∞ln⁡T(w)zw2−z2dw

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)=1−2∫01Ψ(μ)dμ−2∫01μ2Ψ(μ)u−μ2dμ

The above solution is unique and bounded in the interval 0≤z≤1 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+kz1−kz

Properties

  • ∫01H(μ)Ψ(μ)dμ=1−[1−2∫01Ψ(μ)dμ]1/2. For conservative case, this reduces to ∫01Ψ(μ)dμ=12.
  • [1−2∫01Ψ(μ)dμ]1/2∫01H(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=[2∫01Ψ(μ)μ2dμ]1/2.
  • If the characteristic function is Ψ(μ)=a+bμ2, where a,b are two constants(have to satisfy a+b/3≤1/2) and if αn=∫01H(μ)μndμ, n≥1 is the nth moment of the H function, then we have
α0=1+12(aα02+bα12)

and

(a+bμ2)∫01H(μ′)μ+μ′dμ′=H(μ)−1μH(μ)−b(α1−μα0)

See also

References

  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).