Three-dimensional heat conduction boundary value problem

Let us consider the three-dimensional nonsymmetric heat conduction problem in a ball of radius RR. The heat conduction equation (1.8) in spherical coordinates takes the form

T(r,θ,ϕ,t)t\displaystyle \frac{\partial T(r, \theta, \phi, t)}{\partial t} =a22T(r,θ,ϕ,t)r2\displaystyle = a^2 \cdot \frac{\partial^2 T(r, \theta, \phi, t)}{\partial r^2} +2a2rT(r,θ,ϕ,t)r\displaystyle + \frac{2 \cdot a^2}{r} \cdot \frac{\partial T(r, \theta, \phi, t)}{\partial r} +a2r2sin(θ)θ(sin(θ)T(r,θ,ϕ,t)θ)\displaystyle + \frac{a^2}{r^2 \cdot \sin(\theta)} \cdot \frac{\partial}{\partial \theta} \left( \sin(\theta) \cdot \frac{\partial T(r, \theta, \phi, t)}{\partial \theta} \right) +a2r2sin2θ2T(r,θ,ϕ,t)ϕ2\displaystyle + \frac{a^2}{r^2 \cdot \sin^2 \theta} \cdot \frac{\partial^2 T(r, \theta, \phi, t)}{\partial \phi^2} +f(r,θ,ϕ,t),\displaystyle + f(r, \theta, \phi, t),
(2.71)

where rr (0,R)\in (0,R), θ\theta (0,π)\in (0,\pi), ϕ\phi (0,2π)\in (0,2\pi), RR is the radius, T(r,θ,ϕ,t)T(r, \theta, \phi, t) is the temperature, a2a^2 is the thermal diffusivity, f(r,θ,ϕ,t)f(r, \theta, \phi, t) is the heat source density function.

The Dirichlet boundary conditions (1.13) in the three-dimensional case have the form

T(r,θ,ϕ,0)\displaystyle T(r, \theta, \phi, 0) =T0(r,θ,ϕ),\displaystyle = T_0(r, \theta, \phi),T(R,θ,ϕ,t)\displaystyle T(R, \theta, \phi, t) =Φ(θ,ϕ,t),\displaystyle = \Phi(\theta, \phi, t),T(r,0,ϕ,t)\displaystyle |T(r, 0, \phi, t)| <,T(r,π,ϕ,t)\displaystyle < \infty, \quad |T(r, \pi, \phi, t)| <,\displaystyle < \infty,T(r,θ,ϕ,t)\displaystyle T(r, \theta, \phi, t) =T(r,θ,ϕ+2π,t),\displaystyle = T(r, \theta, \phi + 2\pi, t),
(2.72)

where T0(r,θ,ϕ)T_0(r, \theta, \phi) is the initial condition, Φ(θ,ϕ,t)\Phi(\theta, \phi, t) is the boundary condition, which is, of course, periodic in ϕ\phi; at the poles (θ\theta =0= 0 and θ\theta =π= \pi) the boundary conditions are replaced by the requirement that the solution be bounded.

To get rid of the inhomogeneity, we introduce T(r,θ,ϕ,t)T(r, \theta, \phi, t) =T^(r,θ,ϕ,t)= \widehat{T}(r, \theta, \phi, t) +U(θ,ϕ,t)+ U(\theta, \phi, t), let us choose the function U(θ,ϕ,t)U(\theta, \phi, t) =Φ(θ,ϕ,t)= \Phi(\theta, \phi, t), in accordance with (2.2). Then equation (2.71) and the boundary conditions (2.72) take the form

T^(r,θ,ϕ,t)t\displaystyle \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial t} =a22T^(r,θ,ϕ,t)r2\displaystyle = a^2 \cdot \frac{\displaystyle \partial^2 \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial r^2} +2a2rT^(r,θ,ϕ,t)r\displaystyle + \frac{2 \cdot a^2}{r} \cdot \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial r} +a2r2sin(θ)θ(sin(θ)T^(r,θ,ϕ,t)θ)\displaystyle + \frac{a^2}{r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial \theta} \right) +a2r2sin2θ2T^(r,θ,ϕ,t)ϕ2\displaystyle + \frac{a^2}{r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial \phi^2} +f^(r,θ,ϕ,t),\displaystyle + \widehat{f}(r, \theta, \phi, t),T^(r,θ,ϕ,0)\displaystyle \widehat{T}(r, \theta, \phi, 0) =T0(r,θ,ϕ)\displaystyle = T_0(r, \theta, \phi) U(θ,ϕ,0),\displaystyle - U(\theta, \phi, 0),T^(R,θ,ϕ,t)\displaystyle \widehat{T}(R, \theta, \phi, t) =0,\displaystyle = 0,T^(r,0,ϕ,t)\displaystyle |\widehat{T}(r, 0, \phi, t)| <,T^(r,π,ϕ,t)\displaystyle < \infty, \quad |\widehat{T}(r, \pi, \phi, t)| <,\displaystyle < \infty,T^(r,θ,ϕ,t)\displaystyle \widehat{T}(r, \theta, \phi, t) =T^(r,θ,ϕ+2π,t),\displaystyle = \widehat{T}(r, \theta, \phi + 2\pi, t),
(2.73)

where

f^(r,θ,ϕ,t)\displaystyle \widehat{f}(r, \theta, \phi, t) =f(r,θ,ϕ,t)\displaystyle = f(r, \theta, \phi, t) U(θ,ϕ,t)t\displaystyle - \frac{\displaystyle \partial U(\theta, \phi, t)}{\displaystyle \partial t} +a2r2sin(θ)θ(sin(θ)U(θ,ϕ,t)θ)\displaystyle + \frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial U(\theta, \phi, t)}{\displaystyle \partial \theta} \right) +a2r2sin2θ2U(θ,ϕ,t)ϕ2.\displaystyle + \frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 U(\theta, \phi, t)}{\displaystyle \partial \phi^2}.

The Neumann boundary conditions (1.14) in the three-dimensional case have the form

T(r,θ,ϕ,0)\displaystyle T(r, \theta, \phi, 0) =T0(r,θ,ϕ),\displaystyle = T_0(r, \theta, \phi),T(r,θ,ϕ,t)nr=R\displaystyle \frac{\displaystyle \partial T(r, \theta, \phi, t)}{\displaystyle \partial \mathbf{n}} \bigg|_{r=R} =Φ(θ,ϕ,t),\displaystyle = \Phi(\theta, \phi, t),T(r,0,ϕ,t)\displaystyle |T(r, 0, \phi, t)| <,T(r,π,ϕ,t)\displaystyle < \infty, \quad |T(r, \pi, \phi, t)| <,\displaystyle < \infty,T(r,θ,ϕ,t)\displaystyle T(r, \theta, \phi, t) =T(r,θ,ϕ+2π,t),\displaystyle = T(r, \theta, \phi + 2\pi, t),
(2.74)

where T(r,θ,ϕ,t)nr=R\frac{\displaystyle \partial T(r, \theta, \phi, t)}{\displaystyle \partial \mathbf{n}} \bigg|_{r=R} is the normal derivative of the temperature on the sphere of radius RR; the direction of the normal coincides with the direction of the coordinate rr.

To get rid of the inhomogeneity, we introduce T(r,θ,ϕ,t)T(r, \theta, \phi, t) =T^(r,θ,ϕ,t)= \widehat{T}(r, \theta, \phi, t) +U(r,θ,ϕ,t)+ U(r, \theta, \phi, t), let us choose the function U(r,θ,ϕ,t)U(r, \theta, \phi, t) =Φ(θ,ϕ,t)r= \Phi(\theta, \phi, t) \cdot r — it satisfies condition (2.3): U(r,θ,ϕ,t)nr=R\frac{\displaystyle \partial U(r, \theta, \phi, t)}{\displaystyle \partial \mathbf{n}} \bigg|_{r=R} =Φ(θ,ϕ,t)= \Phi(\theta, \phi, t). Then equation (2.71) and the boundary conditions (2.74) take the form

T^(r,θ,ϕ,t)t\displaystyle \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial t} =a22T^(r,θ,ϕ,t)r2\displaystyle = a^2 \cdot \frac{\displaystyle \partial^2 \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial r^2} +2a2rT^(r,θ,ϕ,t)r\displaystyle + \frac{2 \cdot a^2}{r} \cdot \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial r} +a2r2sin(θ)θ(sin(θ)T^(r,θ,ϕ,t)θ)\displaystyle + \frac{a^2}{r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial \theta} \right) +a2r2sin2θ2T^(r,θ,ϕ,t)ϕ2\displaystyle + \frac{a^2}{r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial \phi^2} +f^(r,θ,ϕ,t),\displaystyle + \widehat{f}(r, \theta, \phi, t),T^(r,θ,ϕ,0)\displaystyle \widehat{T}(r, \theta, \phi, 0) =T0(r,θ,ϕ)\displaystyle = T_0(r, \theta, \phi) U(r,θ,ϕ,0),\displaystyle - U(r, \theta, \phi, 0),T^(r,θ,ϕ,t)nr=R\displaystyle \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial \mathbf{n}} \bigg|_{r=R} =0,\displaystyle = 0,T^(r,0,ϕ,t)\displaystyle |\widehat{T}(r, 0, \phi, t)| <,T^(r,π,ϕ,t)\displaystyle < \infty, \quad |\widehat{T}(r, \pi, \phi, t)| <,\displaystyle < \infty,T^(r,θ,ϕ,t)\displaystyle \widehat{T}(r, \theta, \phi, t) =T^(r,θ,ϕ+2π,t),\displaystyle = \widehat{T}(r, \theta, \phi + 2\pi, t),
(2.75)

where

f^(r,θ,ϕ,t)\displaystyle \widehat{f}(r, \theta, \phi, t) =f(r,θ,ϕ,t)\displaystyle = f(r, \theta, \phi, t) U(r,θ,ϕ,t)t\displaystyle - \frac{\displaystyle \partial U(r, \theta, \phi, t)}{\displaystyle \partial t} +a22U(r,θ,ϕ,t)r2\displaystyle + a^2 \cdot \frac{\displaystyle \partial^2 U(r, \theta, \phi, t)}{\displaystyle \partial r^2} +2a2rU(r,θ,ϕ,t)r\displaystyle + \frac{\displaystyle 2 \cdot a^2}{\displaystyle r} \cdot \frac{\displaystyle \partial U(r, \theta, \phi, t)}{\displaystyle \partial r} +a2r2sin(θ)θ(sin(θ)U(r,θ,ϕ,t)θ)\displaystyle + \frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial U(r, \theta, \phi, t)}{\displaystyle \partial \theta} \right) +a2r2sin2θ2U(r,θ,ϕ,t)ϕ2.\displaystyle + \frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 U(r, \theta, \phi, t)}{\displaystyle \partial \phi^2}.

Equation (2.8) takes the form

2Ψ(r,θ,ϕ)r2\displaystyle \frac{\displaystyle \partial^2 \Psi(r, \theta, \phi)}{\displaystyle \partial r^2} +2rΨ(r,θ,ϕ)r\displaystyle + \frac{\displaystyle 2}{\displaystyle r} \cdot \frac{\displaystyle \partial \Psi(r, \theta, \phi)}{\displaystyle \partial r} +1r2sin(θ)θ(sin(θ)Ψ(r,θ,ϕ)θ)\displaystyle + \frac{\displaystyle 1}{\displaystyle r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \Psi(r, \theta, \phi)}{\displaystyle \partial \theta} \right) +1r2sin2θ2Ψ(r,θ,ϕ)ϕ2\displaystyle + \frac{\displaystyle 1}{\displaystyle r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 \Psi(r, \theta, \phi)}{\displaystyle \partial \phi^2} +γ2Ψ(r,θ,ϕ)\displaystyle + \gamma^2 \cdot \Psi(r, \theta, \phi) =0.\displaystyle = 0.
(2.76)

Let us represent the function Ψ(r,θ,ϕ)\Psi(r, \theta, \phi) as a product of three functions Ψ(r,θ,ϕ)\Psi(r, \theta, \phi) =R(r)Θ(θ)Υ(ϕ)= R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi), substitute it into equation (2.76) and carry out the transformations

2(R(r)Θ(θ)Υ(ϕ))r2\displaystyle \frac{\displaystyle \partial^2 (R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial r^2} +2r(R(r)Θ(θ)Υ(ϕ))r\displaystyle + \frac{\displaystyle 2}{\displaystyle r} \cdot \frac{\displaystyle \partial (R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial r} +1r2sin(θ)θ(sin(θ)(R(r)Θ(θ)Υ(ϕ))θ)\displaystyle + \frac{\displaystyle 1}{\displaystyle r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial (R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \theta} \right) +1r2sin2θ2(R(r)Θ(θ)Υ(ϕ))ϕ2\displaystyle + \frac{\displaystyle 1}{\displaystyle r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 (R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \phi^2} +γ2R(r)Θ(θ)Υ(ϕ)\displaystyle + \gamma^2 \cdot R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi) =0,\displaystyle = 0,
Θ(θ)Υ(ϕ)[d2R(r)dr2+2rdR(r)dr]\displaystyle \Theta(\theta) \cdot \Upsilon(\phi) \cdot \left[ \frac{\displaystyle d^2 R(r)}{\displaystyle dr^2} + \frac{\displaystyle 2}{\displaystyle r} \cdot \frac{\displaystyle d R(r)}{\displaystyle dr} \right] +R(r)r2[1sin(θ)θ(sin(θ)(Θ(θ)Υ(ϕ))θ)+1sin2(θ)2(Θ(θ)Υ(ϕ))ϕ2]\displaystyle + \frac{\displaystyle R(r)}{\displaystyle r^2} \cdot \left[ \frac{\displaystyle 1}{\displaystyle \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial (\Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \theta} \right) + \frac{\displaystyle 1}{\displaystyle \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 (\Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \phi^2} \right] +γ2R(r)Θ(θ)Υ(ϕ)\displaystyle + \gamma^2 \cdot R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi) =0,\displaystyle = 0,
Θ(θ)Υ(ϕ)[r2d2R(r)dr2+2rdR(r)dr+r2γ2R(r)]\displaystyle \Theta(\theta) \cdot \Upsilon(\phi) \cdot \left[ r^2 \cdot \frac{\displaystyle d^2 R(r)}{\displaystyle dr^2} + 2 \cdot r \cdot \frac{\displaystyle d R(r)}{\displaystyle dr} + r^2 \cdot \gamma^2 \cdot R(r) \right] +R(r)[1sin(θ)θ(sin(θ)(Θ(θ)Υ(ϕ))θ)+1sin2(θ)2(Θ(θ)Υ(ϕ))ϕ2]\displaystyle + R(r) \cdot \left[ \frac{\displaystyle 1}{\displaystyle \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial (\Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \theta} \right) + \frac{\displaystyle 1}{\displaystyle \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 (\Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \phi^2} \right] =0,\displaystyle = 0,

The expression in the first bracket depends only on rr, the one in the second bracket only on the angles; therefore, dividing by R(r)Θ(θ)Υ(ϕ)R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi), both sides can be set equal to a constant γ12\gamma_1^2 — by analogy with the separation of variables for time and geometry. The equation for the radius takes the form

r2d2R(r)dr2\displaystyle r^2 \cdot \frac{\displaystyle d^2 R(r)}{\displaystyle dr^2} +2rdR(r)dr\displaystyle + 2 \cdot r \cdot \frac{\displaystyle d R(r)}{\displaystyle dr} +(r2γ2γ12)R(r)\displaystyle + \left( r^2 \cdot \gamma^2 - \gamma_1^2 \right) \cdot R(r) =0,\displaystyle = 0,
(2.77)

and continue the transformations

1sin(θ)θ(sin(θ)(Θ(θ)Υ(ϕ))θ)\displaystyle \frac{\displaystyle 1}{\displaystyle \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial (\Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \theta} \right) +1sin2(θ)2(Θ(θ)Υ(ϕ))ϕ2\displaystyle + \frac{\displaystyle 1}{\displaystyle \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 (\Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \phi^2} +γ12Θ(θ)Υ(ϕ)\displaystyle + \gamma_1^2 \cdot \Theta(\theta) \cdot \Upsilon(\phi) =0,\displaystyle = 0,
Υ(ϕ)[1sin(θ)θ(sin(θ)Θ(θ)θ)+γ12Θ(θ)]\displaystyle \Upsilon(\phi) \cdot \left[ \frac{\displaystyle 1}{\displaystyle \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \Theta(\theta)}{\displaystyle \partial \theta} \right) + \gamma_1^2 \cdot \Theta(\theta) \right] +Θ(θ)1sin2(θ)2(Υ(ϕ))ϕ2\displaystyle + \Theta(\theta) \cdot \frac{\displaystyle 1}{\displaystyle \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 (\Upsilon(\phi))}{\displaystyle \partial \phi^2} =0.\displaystyle = 0.

Here the expression in brackets depends only on θ\theta, while the last term depends only on ϕ\phi; therefore, multiplying by sin2(θ)Θ(θ)Υ(ϕ)\frac{\displaystyle \sin^2(\theta)}{\displaystyle \Theta(\theta) \cdot \Upsilon(\phi)}, we separate the variables again with the constant m2m^2 and obtain the equations for the polar and azimuthal angles

1sin(θ)ddθ(sin(θ)dΘ(θ)dθ)\displaystyle \frac{\displaystyle 1}{\displaystyle \sin(\theta)} \cdot \frac{\displaystyle d}{\displaystyle d\theta} \left( \sin(\theta) \cdot \frac{\displaystyle d \Theta(\theta)}{\displaystyle d\theta} \right) +[γ12m2sin2(θ)]Θ(θ)\displaystyle + \left[ \gamma_1^2 - \frac{\displaystyle m^2}{\displaystyle \sin^2(\theta)} \right] \cdot \Theta(\theta) =0,\displaystyle = 0,
(2.78)
d2Υ(ϕ)dϕ2\displaystyle \frac{\displaystyle d^2 \Upsilon(\phi)}{\displaystyle d\phi^2} +m2Υ(ϕ)\displaystyle + m^2 \cdot \Upsilon(\phi) =0.\displaystyle = 0.
(2.79)

The solution of equation (2.79) we already found in the two-dimensional case, so we refer to (2.54). And to solve equation (2.78) let us introduce the substitution zz =cos(θ)= \cos(\theta): for θ\theta (0,π)\in (0, \pi) we have zz (1,1)\in (-1, 1) and dzdz =sin(θ)dθ= - \sin(\theta) \cdot d\theta. Then the equation takes the form

ddz((1z2)dΘ(z)dz)\displaystyle \frac{\displaystyle d}{\displaystyle dz} \left( (1 - z^2) \cdot \frac{\displaystyle d \Theta(z)}{\displaystyle dz} \right) +[γ12m21z2]Θ(z)\displaystyle + \left[ \gamma_1^2 - \frac{\displaystyle m^2}{\displaystyle 1 - z^2} \right] \cdot \Theta(z) =0,\displaystyle = 0, \quad 1\displaystyle -1 <z\displaystyle < z <1.\displaystyle < 1.
(2.80)

This equation is analyzed in the appendix “The Legendre equation”; its solution has the form (E.6)

Θkm(z)\displaystyle \Theta_{km}(z) =Pk(m)(z)\displaystyle = P_k^{(m)}(z) =(1z2)m2dmdzmPk(z),\displaystyle = (1 - z^2)^{\frac{\displaystyle m}{\displaystyle 2}} \cdot \frac{\displaystyle d^m}{\displaystyle dz^m} P_k(z),

where γ1k2\gamma_{1k}^2 =k(k+1)= k \cdot (k + 1) are the eigenvalues, Pk(m)(z)P_k^{(m)}(z) are the associated Legendre polynomials, and nontrivial solutions exist only for mm k\leq k. The norm of the associated Legendre polynomial has the form (F.6). Now let us return to the angle θ\theta, making the inverse substitution

Θkm(θ)\displaystyle \Theta_{km}(\theta) =sinm(θ)dmd(cos(θ))mPk(cos(θ)).\displaystyle = \sin^m(\theta) \cdot \frac{\displaystyle d^m}{\displaystyle d(\cos(\theta))^m} P_k(\cos(\theta)).
(2.81)

Generally speaking, this solution is defined up to a constant factor — let us set it equal to one: it is absorbed into the expansion coefficients anyway. Now let us return to equation (2.77) and rewrite it taking into account γ12\gamma_1^2 =k(k+1)= k \cdot (k + 1)

r2d2R(r)dr2\displaystyle r^2 \cdot \frac{\displaystyle d^2 R(r)}{\displaystyle dr^2} +2rdR(r)dr\displaystyle + 2 \cdot r \cdot \frac{\displaystyle d R(r)}{\displaystyle dr} +(r2γ2k(k+1))R(r)\displaystyle + \left( r^2 \cdot \gamma^2 - k \cdot (k + 1) \right) \cdot R(r) =0.\displaystyle = 0.

This equation is analyzed in the appendix “The Bessel equation in spherical coordinates”: the substitution R(r)R(r) =R^(r)r= \frac{\displaystyle \widehat{R}(r)}{\displaystyle \sqrt{r}} reduces it to the Bessel equation with half-integer index, and the solution has the form (G.2). It should be noted that the solution is bounded at the point rr =0= 0: the Bessel function Jk+1/2(γr)J_{k + 1/2}(\gamma \cdot r) tends to zero no slower than r\sqrt{r}.

Thus, the solutions of equation (2.76) have the form

Ψ1km(r,θ,ϕ)=Akm1rJk+1/2(γr)Pk(m)(cos(θ))sin(mϕ),1mk,k1,\displaystyle \begin{aligned} &\Psi_{1km}(r, \theta, \phi) = A_{km} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi),\\ &1 \leq m \leq k, \quad k \geq 1, \end{aligned}Ψ2km(r,θ,ϕ)=Akm1rJk+1/2(γr)Pk(m)(cos(θ))cos(mϕ),0mk,k0,\displaystyle \begin{aligned} &\Psi_{2km}(r, \theta, \phi) = A_{km} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi),\\ &0 \leq m \leq k, \quad k \geq 0, \end{aligned}
(2.82)

Let us substitute the solutions (2.82) into the boundary conditions (2.73) and obtain

Akm1RJk+1/2(γR)Pk(m)(cos(θ))sin(mϕ)\displaystyle A_{km} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{R}} \cdot J_{k + 1/2}(\gamma \cdot R) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi) =0,1\displaystyle = 0, \quad 1 m\displaystyle \leq m k,k\displaystyle \leq k, \quad k 1,\displaystyle \geq 1,Akm1RJk+1/2(γR)Pk(m)(cos(θ))cos(mϕ)\displaystyle A_{km} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{R}} \cdot J_{k + 1/2}(\gamma \cdot R) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi) =0,0\displaystyle = 0, \quad 0 m\displaystyle \leq m k,k\displaystyle \leq k, \quad k 0.\displaystyle \geq 0.

Clearly, the solution makes sense only when AkmA_{km} 0\neq 0, which is possible only when Jk+1/2(γR)J_{k + 1/2}(\gamma \cdot R) =0= 0. Let us denote the roots of the equation Jk+1/2(μ)J_{k + 1/2}(\mu) =0= 0 by μks\mu_{ks} — then the eigenvalues take the form

Jk+1/2(γR)\displaystyle J_{k + 1/2}(\gamma \cdot R) =0  \displaystyle = 0 \;   γks\displaystyle \Rightarrow\; \gamma_{ks} =μksR,s\displaystyle = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, \quad s (1..).\displaystyle \in (1..\infty).
(2.83)

Zero and negative roots are no good: for μ\mu =0= 0 the eigenfunction Jk+1/2(0r)J_{k + 1/2}(0 \cdot r) 0\equiv 0 — identically zero, which is not an eigenfunction (the index kk +1/2+ 1/2 >0> 0), and negative roots give no new solutions. Therefore we take only the positive roots: μks,s\mu_{ks}, s (1..)\in (1..\infty).

Thus, the eigenvalues and eigenfunctions have the form

γks\displaystyle \gamma_{ks} =μksR,s\displaystyle = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, s (1..),\displaystyle \in (1..\infty),Ψ1kms(r,θ,ϕ)=Akms1rJk+1/2(γksr)Pk(m)(cos(θ))sin(mϕ),1mk,k1,\displaystyle \begin{aligned} &\Psi_{1kms}(r, \theta, \phi) = A_{kms} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi),\\ &1 \leq m \leq k, \quad k \geq 1, \end{aligned}Ψ2kms(r,θ,ϕ)=Akms1rJk+1/2(γksr)Pk(m)(cos(θ))cos(mϕ),0mk,k0,\displaystyle \begin{aligned} &\Psi_{2kms}(r, \theta, \phi) = A_{kms} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi),\\ &0 \leq m \leq k, \quad k \geq 0, \end{aligned}
(2.84)

where AkmsA_{kms} is an arbitrary constant factor: the eigenfunction is defined up to it. Let us set AkmsA_{kms} =1= 1 — this factor is absorbed into the expansion coefficients anyway, as in the general solution.

To expand functions into a Fourier series in Ψ1kms(r,θ,ϕ)\Psi_{1kms}(r, \theta, \phi) and Ψ2kms(r,θ,ϕ)\Psi_{2kms}(r, \theta, \phi) we need to compute the norms Ψ1kms(r,θ,ϕ)2\|\Psi_{1kms}(r, \theta, \phi)\|^2 and Ψ2kms(r,θ,ϕ)2\|\Psi_{2kms}(r, \theta, \phi)\|^2; the weight for spherical coordinates is ρ(r,θ,ϕ)\rho(r, \theta, \phi) =r2sin(θ)= r^2 \cdot \sin(\theta).

Ψ1kms2\displaystyle \|\Psi_{1kms}\|^2 =0RrJk+1/22(γksr)dr0π[Pk(m)(cosθ)]2sin(θ)dθ02πsin2(mϕ)dϕ,1\displaystyle = \int_0^R r \cdot J_{k + 1/2}^2(\gamma_{ks} \cdot r) \,dr \int_0^{\pi} \left[P_k^{(m)}(\cos\theta)\right]^2 \sin(\theta) \,d\theta \cdot \cdot \int_0^{2\pi} \sin^2(m\phi) \,d\phi, \quad 1 m\displaystyle \leq m k,k\displaystyle \leq k, \quad k 1,s\displaystyle \geq 1, \quad s 1,\displaystyle \geq 1,
Ψ2kms2\displaystyle \|\Psi_{2kms}\|^2 =0RrJk+1/22(γksr)dr0π[Pk(m)(cosθ)]2sin(θ)dθ02πcos2(mϕ)dϕ,0\displaystyle = \int_0^R r \cdot J_{k + 1/2}^2(\gamma_{ks} \cdot r) \,dr \int_0^{\pi} \left[P_k^{(m)}(\cos\theta)\right]^2 \sin(\theta) \,d\theta \cdot \cdot \int_0^{2\pi} \cos^2(m\phi) \,d\phi, \quad 0 m\displaystyle \leq m k,k\displaystyle \leq k, \quad k 0,s\displaystyle \geq 0, \quad s 1.\displaystyle \geq 1.

The integral over the azimuthal angle ϕ\phi was computed in (2.59), the integral over the radius is the same as in the Dirichlet problem for the disk: after the substitution xx =γksr= \gamma_{ks} \cdot r it is evaluated by formula (C.6), and the integral over the angle θ\theta after the substitution zz =cos(θ)= \cos(\theta) is exactly the norm of the associated Legendre polynomial (F.6). Let us put it all together

Ψ1kms(r,θ,ϕ)2\displaystyle \|\Psi_{1kms}(r, \theta, \phi)\|^2 =πR22k+1(k+m)!(km)!Jk+3/22(μks),\displaystyle = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}),Ψ2kms(r,θ,ϕ)2\displaystyle \|\Psi_{2kms}(r, \theta, \phi)\|^2 ={2πR22k+1(k+m)!(km)!Jk+3/22(μks),m=0,πR22k+1(k+m)!(km)!Jk+3/22(μks),m1.\displaystyle = \begin{cases} \frac{\displaystyle 2 \cdot \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}), & m = 0, \\ \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}), & m \geq 1 \end{cases}.
(2.85)

Now let us substitute the solution (2.82) into the boundary conditions (2.75); since the direction of the normal coincides with the direction of the coordinate rr, we obtain

Akm[12RRJk+1/2(γR)+γRJk+1/2(γR)]Pk(m)(cos(θ))sin(mϕ)=0,1mk,k1,\displaystyle \begin{aligned} &A_{km} \cdot \left[ - \frac{\displaystyle 1}{\displaystyle 2 \cdot R \cdot \sqrt{R}} \cdot J_{k + 1/2}(\gamma \cdot R) + \frac{\displaystyle \gamma}{\displaystyle \sqrt{R}} \cdot J_{k + 1/2}'(\gamma \cdot R) \right] \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi) = 0,\\ &1 \leq m \leq k, \quad k \geq 1, \end{aligned}Akm[12RRJk+1/2(γR)+γRJk+1/2(γR)]Pk(m)(cos(θ))cos(mϕ)=0,0mk,k0,\displaystyle \begin{aligned} &A_{km} \cdot \left[ - \frac{\displaystyle 1}{\displaystyle 2 \cdot R \cdot \sqrt{R}} \cdot J_{k + 1/2}(\gamma \cdot R) + \frac{\displaystyle \gamma}{\displaystyle \sqrt{R}} \cdot J_{k + 1/2}'(\gamma \cdot R) \right] \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi) = 0,\\ &0 \leq m \leq k, \quad k \geq 0, \end{aligned}

Clearly, the solution makes sense only when AkmA_{km} 0\neq 0, which is possible only when γJk+1/2(γR)\gamma \cdot J_{k + 1/2}'(\gamma \cdot R) =12RJk+1/2(γR)= \frac{\displaystyle 1}{\displaystyle 2 \cdot R} \cdot J_{k + 1/2}(\gamma \cdot R). Let us denote the roots of the equation Jk+1/2(μ)J_{k + 1/2}'(\mu) =12μJk+1/2(μ)= \frac{\displaystyle 1}{\displaystyle 2 \cdot \mu} \cdot J_{k + 1/2}(\mu) by μks\mu_{ks} — then the eigenvalues take the form

Jk+1/2(μks)\displaystyle J_{k + 1/2}'(\mu_{ks}) =12μksJk+1/2(μks)  \displaystyle = \frac{\displaystyle 1}{\displaystyle 2 \cdot \mu_{ks}} \cdot J_{k + 1/2}(\mu_{ks}) \;   γks\displaystyle \Rightarrow\; \gamma_{ks} =μksR,s\displaystyle = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, \quad s (1..).\displaystyle \in (1..\infty).
(2.86)

Here, unlike the Dirichlet problem, the zero mode survives: for kk =0= 0 the radial solution is the spherical Bessel function j0(γr)j_0(\gamma \cdot r) =sin(γr)γr= \frac{\displaystyle \sin(\gamma \cdot r)}{\displaystyle \gamma \cdot r}, and zero is a root of the Neumann condition (j0(0)j_0'(0) =0= 0); it corresponds to γ\gamma =0= 0 and the eigenfunction Ψ(r,θ,ϕ)\Psi(r, \theta, \phi) =1= 1 — a nonzero constant, that is, a fully fledged eigenfunction (the constant mode). We will count it as the first root: μ01\mu_{01} =0= 0. For kk 1\geq 1 the zero root gives no eigenfunction (jk(0)j_k(0) =0= 0), so there we still take only the positive roots.

Thus, the eigenvalues and eigenfunctions have the form

γks\displaystyle \gamma_{ks} =μksR,s\displaystyle = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, s (1..),μ01\displaystyle \in (1..\infty), \quad \mu_{01} =0,\displaystyle = 0,Ψ1kms(r,θ,ϕ)=Akms1rJk+1/2(γksr)Pk(m)(cos(θ))sin(mϕ),1mk,k1,\displaystyle \begin{aligned} &\Psi_{1kms}(r, \theta, \phi) = A_{kms} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi),\\ &1 \leq m \leq k, \quad k \geq 1, \end{aligned}Ψ2kms(r,θ,ϕ)=Akms1rJk+1/2(γksr)Pk(m)(cos(θ))cos(mϕ),0mk,k0,\displaystyle \begin{aligned} &\Psi_{2kms}(r, \theta, \phi) = A_{kms} \cdot \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi),\\ &0 \leq m \leq k, \quad k \geq 0, \end{aligned}
(2.87)

where AkmsA_{kms} is an arbitrary constant factor; as before, we set it equal to one.

We compute the norms of the eigenfunctions in the same way as in the Dirichlet problem: the integrals over the angles remain the same, while the integral over the radius takes a different value — we use formula (H.2) to compute the norm

0RrJk+1/22(γksr)dr\displaystyle \int_0^{R} r \cdot J_{k + 1/2}^2(\gamma_{ks} \cdot r) \,dr =R22[1k(k+1)μks2]Jk+1/22(μks).\displaystyle = \frac{\displaystyle R^2}{\displaystyle 2} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}).

The special case μ01\mu_{01} =0= 0 (for γ01\gamma_{01} =0= 0 the eigenfunction Ψ2001(r,θ,ϕ)\Psi_{2001}(r, \theta, \phi) =1= 1) we compute separately

Ψ2001(r,θ,ϕ)2\displaystyle \|\Psi_{2001}(r, \theta, \phi)\|^2 =0R0π02π1r2sin(θ)drdθdϕ\displaystyle = \int_0^R \int_0^{\pi} \int_0^{2\pi} 1 \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi =4πR33.\displaystyle = \frac{\displaystyle 4 \cdot \pi \cdot R^3}{\displaystyle 3}.
(2.88)

The norms Ψ1kms(r,θ,ϕ)2\|\Psi_{1kms}(r, \theta, \phi)\|^2 and Ψ2kms(r,θ,ϕ)2\|\Psi_{2kms}(r, \theta, \phi)\|^2 have the form

Ψ1kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),Ψ2kms(r,θ,ϕ)2=2πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),m=0,Ψ2kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),m1.\begin{aligned} &\|\Psi_{1kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}),\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle 2 \cdot \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}), \quad m = 0,\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}), \quad m \geq 1. \end{aligned}
(2.89)

The final solution of the three-dimensional Dirichlet boundary value problem with inhomogeneous boundary conditions takes the form

U(θ,ϕ,t)=Φ(θ,ϕ,t),T^(r,θ,ϕ,0)=T0(r,θ,ϕ)U(θ,ϕ,0),f^(r,θ,ϕ,t)=f(r,θ,ϕ,t)Φ(θ,ϕ,t)t+a2r2sin(θ)θ(sin(θ)Φ(θ,ϕ,t)θ)+a2r2sin2(θ)2Φ(θ,ϕ,t)ϕ2,γks=μksR,Jk+1/2(μks)=0,k(0..),s(1..),Ψ1kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))sin(mϕ),1mk,Ψ2kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))cos(mϕ),0mk,Ψ1kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)!Jk+3/22(μks),Ψ2kms(r,θ,ϕ)2=2πR22k+1(k+m)!(km)!Jk+3/22(μks),m=0,Ψ2kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)!Jk+3/22(μks),m1,T01kms=0R0π02πT^(r,θ,ϕ,0)Ψ1kms(r,θ,ϕ)r2sin(θ)drdθdϕ,T02kms=0R0π02πT^(r,θ,ϕ,0)Ψ2kms(r,θ,ϕ)r2sin(θ)drdθdϕ,f1kms(t)=0R0π02πf^(r,θ,ϕ,t)Ψ1kms(r,θ,ϕ)r2sin(θ)drdθdϕ,f2kms(t)=0R0π02πf^(r,θ,ϕ,t)Ψ2kms(r,θ,ϕ)r2sin(θ)drdθdϕ,T^(r,θ,ϕ,t)=k=1m=1ks=1Ψ1kms(r,θ,ϕ)Ψ1kms(r,θ,ϕ)2ea2γks2t[T01kms+0tea2γks2τf1kms(τ)dτ]+k=0m=0ks=1Ψ2kms(r,θ,ϕ)Ψ2kms(r,θ,ϕ)2ea2γks2t[T02kms+0tea2γks2τf2kms(τ)dτ],T(r,θ,ϕ,t)=U(θ,ϕ,t)+T^(r,θ,ϕ,t).\begin{aligned} &U(\theta, \phi, t) = \Phi(\theta, \phi, t),\\ &\widehat{T}(r, \theta, \phi, 0) = T_0(r, \theta, \phi) - U(\theta, \phi, 0),\\ &\widehat{f}(r, \theta, \phi, t) = f(r, \theta, \phi, t) - \frac{\displaystyle \partial \Phi(\theta, \phi, t)}{\displaystyle \partial t} + \frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \Phi(\theta, \phi, t)}{\displaystyle \partial \theta} \right) +\\ &\frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 \Phi(\theta, \phi, t)}{\displaystyle \partial \phi^2},\\ &\gamma_{ks} = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, \quad J_{k + 1/2}(\mu_{ks}) = 0, \quad k \in (0..\infty), \quad s \in (1..\infty),\\ &\Psi_{1kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi), \quad 1 \leq m \leq k,\\ &\Psi_{2kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi), \quad 0 \leq m \leq k,\\ &\|\Psi_{1kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}),\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle 2 \cdot \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}), \quad m = 0,\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}), \quad m \geq 1,\\ &T_{01kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{T}(r, \theta, \phi, 0) \cdot \Psi_{1kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &T_{02kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{T}(r, \theta, \phi, 0) \cdot \Psi_{2kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &f_{1kms}(t) = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi, t) \cdot \Psi_{1kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &f_{2kms}(t) = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi, t) \cdot \Psi_{2kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &\widehat{T}(r, \theta, \phi, t) =\\ &\sum_{k=1}^{\infty} \sum_{m=1}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{1kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{1kms}(r, \theta, \phi)\|^2} \cdot e^{- a^2 \cdot \gamma_{ks}^2 \cdot t} \cdot \left[ T_{01kms} + \int_0^t e^{a^2 \cdot \gamma_{ks}^2 \cdot \tau} \cdot f_{1kms}(\tau) \,d\tau \right] +\\ &\sum_{k=0}^{\infty} \sum_{m=0}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{2kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{2kms}(r, \theta, \phi)\|^2} \cdot e^{- a^2 \cdot \gamma_{ks}^2 \cdot t} \cdot \left[ T_{02kms} + \int_0^t e^{a^2 \cdot \gamma_{ks}^2 \cdot \tau} \cdot f_{2kms}(\tau) \,d\tau \right],\\ &T(r, \theta, \phi, t) = U(\theta, \phi, t) + \widehat{T}(r, \theta, \phi, t). \end{aligned}
(2.90)

In the Neumann problem, unlike the Dirichlet one, the spectrum contains the zero mode (γ01\gamma_{01} =0= 0, Ψ2001(r,θ,ϕ)\Psi_{2001}(r, \theta, \phi) =1= 1) — the case γ\gamma =0= 0, which in the general solution (2.18) was set aside for separate consideration; it is precisely what gives the non-decaying term — the term with kk =0,m= 0, m =0,s= 0, s =1= 1 in the second sum. The final solution of the three-dimensional Neumann boundary value problem with inhomogeneous boundary conditions takes the form

U(r,θ,ϕ,t)=Φ(θ,ϕ,t)r,T^(r,θ,ϕ,0)=T0(r,θ,ϕ)U(r,θ,ϕ,0),f^(r,θ,ϕ,t)=f(r,θ,ϕ,t)rΦ(θ,ϕ,t)t+2a2Φ(θ,ϕ,t)r+a2rsin(θ)θ(sin(θ)Φ(θ,ϕ,t)θ)+a2rsin2(θ)2Φ(θ,ϕ,t)ϕ2,γks=μksR,Jk+1/2(μks)=12μksJk+1/2(μks),μ01=0,k(0..),s(1..),Ψ1kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))sin(mϕ),1mk,Ψ2kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))cos(mϕ),0mk,Ψ1kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),Ψ2kms(r,θ,ϕ)2=2πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),m=0,Ψ2kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),m1,Ψ2001(r,θ,ϕ)2=4πR33,T01kms=0R0π02πT^(r,θ,ϕ,0)Ψ1kms(r,θ,ϕ)r2sin(θ)drdθdϕ,T02kms=0R0π02πT^(r,θ,ϕ,0)Ψ2kms(r,θ,ϕ)r2sin(θ)drdθdϕ,f1kms(t)=0R0π02πf^(r,θ,ϕ,t)Ψ1kms(r,θ,ϕ)r2sin(θ)drdθdϕ,f2kms(t)=0R0π02πf^(r,θ,ϕ,t)Ψ2kms(r,θ,ϕ)r2sin(θ)drdθdϕ,T^(r,θ,ϕ,t)=k=1m=1ks=1Ψ1kms(r,θ,ϕ)Ψ1kms(r,θ,ϕ)2ea2γks2t[T01kms+0tea2γks2τf1kms(τ)dτ]+k=0m=0ks=1Ψ2kms(r,θ,ϕ)Ψ2kms(r,θ,ϕ)2ea2γks2t[T02kms+0tea2γks2τf2kms(τ)dτ],T(r,θ,ϕ,t)=U(r,θ,ϕ,t)+T^(r,θ,ϕ,t).\begin{aligned} &U(r, \theta, \phi, t) = \Phi(\theta, \phi, t) \cdot r,\\ &\widehat{T}(r, \theta, \phi, 0) = T_0(r, \theta, \phi) - U(r, \theta, \phi, 0),\\ &\widehat{f}(r, \theta, \phi, t) = f(r, \theta, \phi, t) - r \cdot \frac{\displaystyle \partial \Phi(\theta, \phi, t)}{\displaystyle \partial t} + \frac{\displaystyle 2 \cdot a^2 \cdot \Phi(\theta, \phi, t)}{\displaystyle r} +\\ &\frac{\displaystyle a^2}{\displaystyle r \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \Phi(\theta, \phi, t)}{\displaystyle \partial \theta} \right) +\\ &\frac{\displaystyle a^2}{\displaystyle r \cdot \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 \Phi(\theta, \phi, t)}{\displaystyle \partial \phi^2},\\ &\gamma_{ks} = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, \quad J_{k + 1/2}'(\mu_{ks}) = \frac{\displaystyle 1}{\displaystyle 2 \cdot \mu_{ks}} \cdot J_{k + 1/2}(\mu_{ks}), \quad \mu_{01} = 0,\\ &k \in (0..\infty), \quad s \in (1..\infty),\\ &\Psi_{1kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi), \quad 1 \leq m \leq k,\\ &\Psi_{2kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi), \quad 0 \leq m \leq k,\\ &\|\Psi_{1kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}),\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle 2 \cdot \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}), \quad m = 0,\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}), \quad m \geq 1,\\ &\|\Psi_{2001}(r, \theta, \phi)\|^2 = \frac{\displaystyle 4 \cdot \pi \cdot R^3}{\displaystyle 3},\\ &T_{01kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{T}(r, \theta, \phi, 0) \cdot \Psi_{1kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &T_{02kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{T}(r, \theta, \phi, 0) \cdot \Psi_{2kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &f_{1kms}(t) = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi, t) \cdot \Psi_{1kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &f_{2kms}(t) = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi, t) \cdot \Psi_{2kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &\widehat{T}(r, \theta, \phi, t) =\\ &\sum_{k=1}^{\infty} \sum_{m=1}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{1kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{1kms}(r, \theta, \phi)\|^2} \cdot e^{- a^2 \cdot \gamma_{ks}^2 \cdot t} \cdot \left[ T_{01kms} + \int_0^t e^{a^2 \cdot \gamma_{ks}^2 \cdot \tau} \cdot f_{1kms}(\tau) \,d\tau \right] +\\ &\sum_{k=0}^{\infty} \sum_{m=0}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{2kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{2kms}(r, \theta, \phi)\|^2} \cdot e^{- a^2 \cdot \gamma_{ks}^2 \cdot t} \cdot \left[ T_{02kms} + \int_0^t e^{a^2 \cdot \gamma_{ks}^2 \cdot \tau} \cdot f_{2kms}(\tau) \,d\tau \right],\\ &T(r, \theta, \phi, t) = U(r, \theta, \phi, t) + \widehat{T}(r, \theta, \phi, t). \end{aligned}
(2.91)

To obtain the stationary solutions, we let time tend to infinity in the solutions found (tt \to \infty), as was done for the general case in (2.18). The term with the initial condition vanishes, since ea2γks2te^{- a^2 \cdot \gamma_{ks}^2 \cdot t} 0\to 0; the sources and boundary conditions stop depending on time, and the time integral for γks\gamma_{ks} 0\neq 0 gives the factor 1a2γks2\frac{1}{a^2 \cdot \gamma_{ks}^2}:

0tea2γks2(tτ)dτ\displaystyle \int_0^t e^{- a^2 \cdot \gamma_{ks}^2 \cdot (t - \tau)} \,d\tau =1a2γks2(1ea2γks2t)\displaystyle = \frac{\displaystyle 1}{\displaystyle a^2 \cdot \gamma_{ks}^2} \cdot (1 - e^{- a^2 \cdot \gamma_{ks}^2 \cdot t}) 1a2γks2ast\displaystyle \rightarrow \frac{\displaystyle 1}{\displaystyle a^2 \cdot \gamma_{ks}^2} \quad \text{as} \quad t ,γks\displaystyle \rightarrow \infty, \quad \gamma_{ks} 0.\displaystyle \neq 0.

The stationary solution of the three-dimensional Dirichlet boundary value problem takes the form

U(θ,ϕ)=Φ(θ,ϕ),f^(r,θ,ϕ)=f(r,θ,ϕ)+a2r2sin(θ)θ(sin(θ)Φ(θ,ϕ)θ)+a2r2sin2(θ)2Φ(θ,ϕ)ϕ2,γks=μksR,Jk+1/2(μks)=0,k(0..),s(1..),Ψ1kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))sin(mϕ),1mk,Ψ2kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))cos(mϕ),0mk,Ψ1kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)!Jk+3/22(μks),Ψ2kms(r,θ,ϕ)2=2πR22k+1(k+m)!(km)!Jk+3/22(μks),m=0,Ψ2kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)!Jk+3/22(μks),m1,f1kms=0R0π02πf^(r,θ,ϕ)Ψ1kms(r,θ,ϕ)r2sin(θ)drdθdϕ,f2kms=0R0π02πf^(r,θ,ϕ)Ψ2kms(r,θ,ϕ)r2sin(θ)drdθdϕ,T(r,θ,ϕ)=U(θ,ϕ)+k=1m=1ks=1Ψ1kms(r,θ,ϕ)Ψ1kms(r,θ,ϕ)2f1kmsa2γks2+k=0m=0ks=1Ψ2kms(r,θ,ϕ)Ψ2kms(r,θ,ϕ)2f2kmsa2γks2.\begin{aligned} &U(\theta, \phi) = \Phi(\theta, \phi),\\ &\widehat{f}(r, \theta, \phi) = f(r, \theta, \phi) + \frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \Phi(\theta, \phi)}{\displaystyle \partial \theta} \right) + \frac{\displaystyle a^2}{\displaystyle r^2 \cdot \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 \Phi(\theta, \phi)}{\displaystyle \partial \phi^2},\\ &\gamma_{ks} = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, \quad J_{k + 1/2}(\mu_{ks}) = 0, \quad k \in (0..\infty), \quad s \in (1..\infty),\\ &\Psi_{1kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi), \quad 1 \leq m \leq k,\\ &\Psi_{2kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi), \quad 0 \leq m \leq k,\\ &\|\Psi_{1kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}),\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle 2 \cdot \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}), \quad m = 0,\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot J_{k + 3/2}^2(\mu_{ks}), \quad m \geq 1,\\ &f_{1kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi) \cdot \Psi_{1kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &f_{2kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi) \cdot \Psi_{2kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &T(r, \theta, \phi) = U(\theta, \phi) + \sum_{k=1}^{\infty} \sum_{m=1}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{1kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{1kms}(r, \theta, \phi)\|^2} \cdot \frac{\displaystyle f_{1kms}}{\displaystyle a^2 \cdot \gamma_{ks}^2} +\\ &\sum_{k=0}^{\infty} \sum_{m=0}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{2kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{2kms}(r, \theta, \phi)\|^2} \cdot \frac{\displaystyle f_{2kms}}{\displaystyle a^2 \cdot \gamma_{ks}^2}. \end{aligned}
(2.92)

The stationary solution of the three-dimensional Neumann boundary value problem is not so simple. Unlike the Dirichlet problem, the purely Neumann stationary problem is not always solvable. The reduced function T^(r,θ,ϕ)\widehat{T}(r, \theta, \phi) satisfies the homogeneous Neumann conditions and the stationary equation a2ΔT^(r,θ,ϕ)a^2 \cdot \Delta \widehat{T}(r, \theta, \phi) +f^(r,θ,ϕ)+ \widehat{f}(r, \theta, \phi) =0= 0. Let us integrate it over the domain:

0=0R0π02π(a2ΔT^+f^)r2sin(θ)drdθdϕ=a2r=RT^ndS+0R0π02πf^r2sin(θ)drdθdϕ=0R0π02πf^r2sin(θ)drdθdϕ.\begin{split} &0 = \int_0^R \int_0^{\pi} \int_0^{2\pi} \left( a^2 \cdot \Delta \widehat{T} + \widehat{f} \right) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi =\\ &a^2 \cdot \oint_{r=R} \frac{\displaystyle \partial \widehat{T}}{\displaystyle \partial \mathbf{n}} \,dS + \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f} \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f} \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi. \end{split}

The boundary integral vanished due to the homogeneous Neumann conditions, and what remains is the solvability condition (2.22): 0R0π02πf^(r,θ,ϕ)r2sin(θ)drdθdϕ\int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi =0= 0 — the total reduced source over the domain must vanish (otherwise heat accumulates and there is no steady state). When it holds, the solution is defined only up to an arbitrary additive constant CC: it corresponds to the zero mode (γ01\gamma_{01} =0= 0, Ψ2001(r,θ,ϕ)\Psi_{2001}(r, \theta, \phi) =1= 1), whose amplitude is not fixed by the stationary equation. With this caveat the solution takes the form

U(r,θ,ϕ)=Φ(θ,ϕ)r,f^(r,θ,ϕ)=f(r,θ,ϕ)+2a2Φ(θ,ϕ)r+a2rsin(θ)θ(sin(θ)Φ(θ,ϕ)θ)+a2rsin2(θ)2Φ(θ,ϕ)ϕ2,γks=μksR,Jk+1/2(μks)=12μksJk+1/2(μks),μks>0,k(0..),s(1..),Ψ1kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))sin(mϕ),1mk,Ψ2kms(r,θ,ϕ)=1rJk+1/2(γksr)Pk(m)(cos(θ))cos(mϕ),0mk,Ψ1kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),Ψ2kms(r,θ,ϕ)2=2πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),m=0,Ψ2kms(r,θ,ϕ)2=πR22k+1(k+m)!(km)![1k(k+1)μks2]Jk+1/22(μks),m1,f1kms=0R0π02πf^(r,θ,ϕ)Ψ1kms(r,θ,ϕ)r2sin(θ)drdθdϕ,f2kms=0R0π02πf^(r,θ,ϕ)Ψ2kms(r,θ,ϕ)r2sin(θ)drdθdϕ,T(r,θ,ϕ)=U(r,θ,ϕ)+k=1m=1ks=1Ψ1kms(r,θ,ϕ)Ψ1kms(r,θ,ϕ)2f1kmsa2γks2+k=0m=0ks=1Ψ2kms(r,θ,ϕ)Ψ2kms(r,θ,ϕ)2f2kmsa2γks2+C,C=const.\begin{aligned} &U(r, \theta, \phi) = \Phi(\theta, \phi) \cdot r,\\ &\widehat{f}(r, \theta, \phi) = f(r, \theta, \phi) + \frac{\displaystyle 2 \cdot a^2 \cdot \Phi(\theta, \phi)}{\displaystyle r} +\\ &\frac{\displaystyle a^2}{\displaystyle r \cdot \sin(\theta)} \cdot \frac{\displaystyle \partial}{\displaystyle \partial \theta} \left( \sin(\theta) \cdot \frac{\displaystyle \partial \Phi(\theta, \phi)}{\displaystyle \partial \theta} \right) + \frac{\displaystyle a^2}{\displaystyle r \cdot \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 \Phi(\theta, \phi)}{\displaystyle \partial \phi^2},\\ &\gamma_{ks} = \frac{\displaystyle \mu_{ks}}{\displaystyle R}, \quad J_{k + 1/2}'(\mu_{ks}) = \frac{\displaystyle 1}{\displaystyle 2 \cdot \mu_{ks}} \cdot J_{k + 1/2}(\mu_{ks}), \quad \mu_{ks} > 0,\\ &k \in (0..\infty), \quad s \in (1..\infty),\\ &\Psi_{1kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \sin(m \cdot \phi), \quad 1 \leq m \leq k,\\ &\Psi_{2kms}(r, \theta, \phi) = \frac{\displaystyle 1}{\displaystyle \sqrt{r}} \cdot J_{k + 1/2}(\gamma_{ks} \cdot r) \cdot P_k^{(m)}(\cos(\theta)) \cdot \cos(m \cdot \phi), \quad 0 \leq m \leq k,\\ &\|\Psi_{1kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}),\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle 2 \cdot \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}), \quad m = 0,\\ &\|\Psi_{2kms}(r, \theta, \phi)\|^2 = \frac{\displaystyle \pi \cdot R^2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!} \cdot \left[ 1 - \frac{\displaystyle k \cdot (k+1)}{\displaystyle \mu_{ks}^2} \right] \cdot J_{k + 1/2}^2(\mu_{ks}), \quad m \geq 1,\\ &f_{1kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi) \cdot \Psi_{1kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &f_{2kms} = \int_0^R \int_0^{\pi} \int_0^{2\pi} \widehat{f}(r, \theta, \phi) \cdot \Psi_{2kms}(r, \theta, \phi) \cdot r^2 \cdot \sin(\theta) \,dr \,d\theta \,d\phi,\\ &T(r, \theta, \phi) = U(r, \theta, \phi) + \sum_{k=1}^{\infty} \sum_{m=1}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{1kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{1kms}(r, \theta, \phi)\|^2} \cdot \frac{\displaystyle f_{1kms}}{\displaystyle a^2 \cdot \gamma_{ks}^2} +\\ &\sum_{k=0}^{\infty} \sum_{m=0}^{k} \sum_{s=1}^{\infty} \frac{\displaystyle \Psi_{2kms}(r, \theta, \phi)}{\displaystyle \|\Psi_{2kms}(r, \theta, \phi)\|^2} \cdot \frac{\displaystyle f_{2kms}}{\displaystyle a^2 \cdot \gamma_{ks}^2} + C, \quad C = \text{const}. \end{aligned}
(2.93)