Let us consider the three-dimensional nonsymmetric heat conduction problem in a ball of radius R R . The heat conduction equation (1.8 ∂ T ( M , t ) ∂ t \displaystyle \frac{\partial T(M, t)}{\partial t} = a 2 ⋅ Δ T ( M , t ) \displaystyle = a^2 \cdot \Delta T(M, t) + f ( M , t ) , \displaystyle + f(M, t), ) in spherical coordinates takes the form
where r r ∈ ( 0 , R ) \in (0,R) , θ \theta ∈ ( 0 , π ) \in (0,\pi) , ϕ \phi ∈ ( 0 , 2 π ) \in (0,2\pi) , R R is the radius, T ( r , θ , ϕ , t ) T(r, \theta, \phi, t) is the temperature, a 2 a^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 T ( M , t ) \displaystyle T(M, t) = Φ ( M , t ) , M \displaystyle = \Phi(M, t), \quad M ∈ S . \displaystyle \in S. ) in the three-dimensional case have the form
where T 0 ( 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 T ^ ( M , t ) \displaystyle \widehat{T}(M, t) + U ( M , t ) \displaystyle + U(M, t) = Φ ( M , t ) , T ^ ( M , t ) \displaystyle = \Phi(M, t), \quad \widehat{T}(M, t) = 0 \displaystyle = 0 \; ⇒ U ( M , t ) \displaystyle \Rightarrow\; U(M, t) = Φ ( M , t ) , M \displaystyle = \Phi(M, t), \quad M ∈ S . \displaystyle \in S. ). Then equation (2.71 ∂ T ( r , θ , ϕ , t ) ∂ t \displaystyle \frac{\partial T(r, \theta, \phi, t)}{\partial t} = a 2 ⋅ ∂ 2 T ( r , θ , ϕ , t ) ∂ r 2 \displaystyle = a^2 \cdot \frac{\partial^2 T(r, \theta, \phi, t)}{\partial r^2} + 2 ⋅ a 2 r ⋅ ∂ T ( r , θ , ϕ , t ) ∂ r \displaystyle + \frac{2 \cdot a^2}{r} \cdot \frac{\partial T(r, \theta, \phi, t)}{\partial r} + a 2 r 2 ⋅ sin ( 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) + a 2 r 2 ⋅ sin 2 θ ⋅ ∂ 2 T ( r , θ , ϕ , t ) ∂ ϕ 2 \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), ) and the boundary conditions (2.72 T ( r , θ , ϕ , 0 ) \displaystyle T(r, \theta, \phi, 0) = T 0 ( 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 + 2 π , t ) , \displaystyle = T(r, \theta, \phi + 2\pi, t), ) take the form
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} + a 2 r 2 ⋅ sin ( 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) + a 2 r 2 ⋅ sin 2 θ ⋅ ∂ 2 U ( θ , ϕ , t ) ∂ ϕ 2 . \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 λ ⋅ ∂ T ( M , t ) ∂ n ⃗ \displaystyle \lambda \cdot \frac{\partial T(M, t)}{\partial \vec{n}} = Φ ( M , t ) , M \displaystyle = \Phi(M, t), \quad M ∈ S , \displaystyle \in S, ) in the three-dimensional case have the form
where ∂ T ( r , θ , ϕ , t ) ∂ n ∣ r = 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 R R ; the direction of the normal coincides with the direction of the coordinate r r .
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 ∂ T ^ ( M , t ) ∂ n ⃗ \displaystyle \frac{\partial \widehat{T}(M, t)}{\partial \vec{n}} + ∂ U ( M , t ) ∂ n ⃗ \displaystyle + \frac{\partial U(M, t)}{\partial \vec{n}} = Φ ( M , t ) , ∂ T ^ ( M , t ) ∂ n ⃗ \displaystyle = \Phi(M, t), \quad \frac{\partial \widehat{T}(M, t)}{\partial \vec{n}} = 0 \displaystyle = 0 \; ⇒ ∂ U ( M , t ) ∂ n ⃗ \displaystyle \Rightarrow\; \frac{\partial U(M, t)}{\partial \vec{n}} = Φ ( M , t ) , M \displaystyle = \Phi(M, t), \quad M ∈ S . \displaystyle \in S. ): ∂ U ( r , θ , ϕ , t ) ∂ n ∣ r = 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 ∂ T ( r , θ , ϕ , t ) ∂ t \displaystyle \frac{\partial T(r, \theta, \phi, t)}{\partial t} = a 2 ⋅ ∂ 2 T ( r , θ , ϕ , t ) ∂ r 2 \displaystyle = a^2 \cdot \frac{\partial^2 T(r, \theta, \phi, t)}{\partial r^2} + 2 ⋅ a 2 r ⋅ ∂ T ( r , θ , ϕ , t ) ∂ r \displaystyle + \frac{2 \cdot a^2}{r} \cdot \frac{\partial T(r, \theta, \phi, t)}{\partial r} + a 2 r 2 ⋅ sin ( 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) + a 2 r 2 ⋅ sin 2 θ ⋅ ∂ 2 T ( r , θ , ϕ , t ) ∂ ϕ 2 \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), ) and the boundary conditions (2.74 T ( r , θ , ϕ , 0 ) \displaystyle T(r, \theta, \phi, 0) = T 0 ( r , θ , ϕ ) , \displaystyle = T_0(r, \theta, \phi), ∂ T ( r , θ , ϕ , t ) ∂ n ∣ r = 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 + 2 π , t ) , \displaystyle = T(r, \theta, \phi + 2\pi, t), ) take the form
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} + a 2 ⋅ ∂ 2 U ( r , θ , ϕ , t ) ∂ r 2 \displaystyle + a^2 \cdot \frac{\displaystyle \partial^2 U(r, \theta, \phi, t)}{\displaystyle \partial r^2} + 2 ⋅ a 2 r ⋅ ∂ U ( 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} + a 2 r 2 ⋅ sin ( 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) + a 2 r 2 ⋅ sin 2 θ ⋅ ∂ 2 U ( r , θ , ϕ , t ) ∂ ϕ 2 . \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 Δ Ψ ( M ) \displaystyle \Delta \Psi(M) + γ 2 ⋅ Ψ ( M ) \displaystyle + \gamma^2 \cdot \Psi(M) = 0. \displaystyle = 0. ) takes the form
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 ∂ 2 Ψ ( r , θ , ϕ ) ∂ r 2 \displaystyle \frac{\displaystyle \partial^2 \Psi(r, \theta, \phi)}{\displaystyle \partial r^2} + 2 r ⋅ ∂ Ψ ( r , θ , ϕ ) ∂ r \displaystyle + \frac{\displaystyle 2}{\displaystyle r} \cdot \frac{\displaystyle \partial \Psi(r, \theta, \phi)}{\displaystyle \partial r} + 1 r 2 ⋅ sin ( 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) + 1 r 2 ⋅ sin 2 θ ⋅ ∂ 2 Ψ ( r , θ , ϕ ) ∂ ϕ 2 \displaystyle + \frac{\displaystyle 1}{\displaystyle r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 \Psi(r, \theta, \phi)}{\displaystyle \partial \phi^2} + γ 2 ⋅ Ψ ( r , θ , ϕ ) \displaystyle + \gamma^2 \cdot \Psi(r, \theta, \phi) = 0. \displaystyle = 0. ) and carry out the transformations
∂ 2 ( R ( r ) ⋅ Θ ( θ ) ⋅ Υ ( ϕ ) ) ∂ r 2 \displaystyle \frac{\displaystyle \partial^2 (R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial r^2} + 2 r ⋅ ∂ ( 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} + 1 r 2 ⋅ sin ( 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) + 1 r 2 ⋅ sin 2 θ ⋅ ∂ 2 ( R ( r ) ⋅ Θ ( θ ) ⋅ Υ ( ϕ ) ) ∂ ϕ 2 \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} + γ 2 ⋅ R ( r ) ⋅ Θ ( θ ) ⋅ Υ ( ϕ ) \displaystyle + \gamma^2 \cdot R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi) = 0 , \displaystyle = 0, Θ ( θ ) ⋅ Υ ( ϕ ) ⋅ [ d 2 R ( r ) d r 2 + 2 r ⋅ d R ( r ) d r ] \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 ) r 2 ⋅ [ 1 sin ( θ ) ⋅ ∂ ∂ θ ( sin ( θ ) ⋅ ∂ ( Θ ( θ ) ⋅ Υ ( ϕ ) ) ∂ θ ) + 1 sin 2 ( θ ) ⋅ ∂ 2 ( Θ ( θ ) ⋅ Υ ( ϕ ) ) ∂ ϕ 2 ] \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] + γ 2 ⋅ R ( r ) ⋅ Θ ( θ ) ⋅ Υ ( ϕ ) \displaystyle + \gamma^2 \cdot R(r) \cdot \Theta(\theta) \cdot \Upsilon(\phi) = 0 , \displaystyle = 0, Θ ( θ ) ⋅ Υ ( ϕ ) ⋅ [ r 2 ⋅ d 2 R ( r ) d r 2 + 2 ⋅ r ⋅ d R ( r ) d r + r 2 ⋅ γ 2 ⋅ R ( 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 ) ⋅ [ 1 sin ( θ ) ⋅ ∂ ∂ θ ( sin ( θ ) ⋅ ∂ ( Θ ( θ ) ⋅ Υ ( ϕ ) ) ∂ θ ) + 1 sin 2 ( θ ) ⋅ ∂ 2 ( Θ ( θ ) ⋅ Υ ( ϕ ) ) ∂ ϕ 2 ] \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 r r , 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 γ 1 2 \gamma_1^2 — by analogy with the separation of variables for time and geometry. The equation for the radius takes the form
and continue the transformations
1 sin ( 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) + 1 sin 2 ( θ ) ⋅ ∂ 2 ( Θ ( θ ) ⋅ Υ ( ϕ ) ) ∂ ϕ 2 \displaystyle + \frac{\displaystyle 1}{\displaystyle \sin^2(\theta)} \cdot \frac{\displaystyle \partial^2 (\Theta(\theta) \cdot \Upsilon(\phi))}{\displaystyle \partial \phi^2} + γ 1 2 ⋅ Θ ( θ ) ⋅ Υ ( ϕ ) \displaystyle + \gamma_1^2 \cdot \Theta(\theta) \cdot \Upsilon(\phi) = 0 , \displaystyle = 0, Υ ( ϕ ) ⋅ [ 1 sin ( θ ) ⋅ ∂ ∂ θ ( sin ( θ ) ⋅ ∂ Θ ( θ ) ∂ θ ) + γ 1 2 ⋅ Θ ( 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 ) ⋅ 1 sin 2 ( θ ) ⋅ ∂ 2 ( Υ ( ϕ ) ) ∂ ϕ 2 \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 sin 2 ( θ ) Θ ( θ ) ⋅ Υ ( ϕ ) \frac{\displaystyle \sin^2(\theta)}{\displaystyle \Theta(\theta) \cdot \Upsilon(\phi)} , we separate the variables again with the constant m 2 m^2 and obtain the equations for the polar and azimuthal angles
The solution of equation (2.79 d 2 Υ ( ϕ ) d ϕ 2 \displaystyle \frac{\displaystyle d^2 \Upsilon(\phi)}{\displaystyle d\phi^2} + m 2 ⋅ Υ ( ϕ ) \displaystyle + m^2 \cdot \Upsilon(\phi) = 0. \displaystyle = 0. ) we already found in the two-dimensional case, so we refer to (2.54 Υ 1 m ( θ ) \displaystyle \Upsilon_{1m}(\theta) = C 1 m ⋅ sin ( m ⋅ θ ) , m \displaystyle = C_{1m} \cdot \sin(m \cdot \theta), m ∈ ( 1.. ∞ ) , \displaystyle \in (1..\infty), Υ 2 m ( θ ) \displaystyle \Upsilon_{2m}(\theta) = C 2 m ⋅ cos ( m ⋅ θ ) , m \displaystyle = C_{2m} \cdot \cos(m \cdot \theta), m ∈ ( 0.. ∞ ) . \displaystyle \in (0..\infty). ). And to solve equation (2.78 1 sin ( θ ) ⋅ d d θ ( sin ( θ ) ⋅ d Θ ( θ ) d θ ) \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) + [ γ 1 2 − m 2 sin 2 ( θ ) ] ⋅ Θ ( θ ) \displaystyle + \left[ \gamma_1^2 - \frac{\displaystyle m^2}{\displaystyle \sin^2(\theta)} \right] \cdot \Theta(\theta) = 0 , \displaystyle = 0, ) let us introduce the substitution z z = cos ( θ ) = \cos(\theta) : for θ \theta ∈ ( 0 , π ) \in (0, \pi) we have z z ∈ ( − 1 , 1 ) \in (-1, 1) and d z dz = − sin ( θ ) ⋅ d θ = - \sin(\theta) \cdot d\theta . Then the equation takes the form
This equation is analyzed in the appendix “The Legendre equation”; its solution has the form (E.6 Θ k m ( z ) \displaystyle \Theta_{km}(z) = P k ( m ) ( z ) \displaystyle = P_k^{(m)}(z) = ( 1 − z 2 ) m 2 ⋅ d m d z m P k ( z ) , \displaystyle = (1 - z^2)^{\frac{\displaystyle m}{\displaystyle 2}} \cdot \frac{\displaystyle d^m}{\displaystyle dz^m} P_k(z), )
Θ k m ( z ) \displaystyle \Theta_{km}(z) = P k ( m ) ( z ) \displaystyle = P_k^{(m)}(z) = ( 1 − z 2 ) m 2 ⋅ d m d z m P k ( z ) , \displaystyle = (1 - z^2)^{\frac{\displaystyle m}{\displaystyle 2}} \cdot \frac{\displaystyle d^m}{\displaystyle dz^m} P_k(z), where γ 1 k 2 \gamma_{1k}^2 = k ⋅ ( k + 1 ) = k \cdot (k + 1) are the eigenvalues, P k ( m ) ( z ) P_k^{(m)}(z) are the associated Legendre polynomials, and nontrivial solutions exist only for m m ≤ k \leq k . The norm of the associated Legendre polynomial has the form (F.6 ∫ − 1 1 [ P k ( m ) ( z ) ] 2 d z \displaystyle \int_{-1}^1 \left[ P_k^{(m)}(z) \right]^2 \,dz = 2 2 ⋅ k + 1 ⋅ ( k + m ) ! ( k − m ) ! , m \displaystyle = \frac{\displaystyle 2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!}, \quad m ≤ k . \displaystyle \leq k. ). Now let us return to the angle θ \theta , making the inverse substitution
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 r 2 ⋅ d 2 R ( r ) d r 2 \displaystyle r^2 \cdot \frac{\displaystyle d^2 R(r)}{\displaystyle dr^2} + 2 ⋅ r ⋅ d R ( r ) d r \displaystyle + 2 \cdot r \cdot \frac{\displaystyle d R(r)}{\displaystyle dr} + ( r 2 ⋅ γ 2 − γ 1 2 ) ⋅ R ( r ) \displaystyle + \left( r^2 \cdot \gamma^2 - \gamma_1^2 \right) \cdot R(r) = 0 , \displaystyle = 0, ) and rewrite it taking into account γ 1 2 \gamma_1^2 = k ⋅ ( k + 1 ) = k \cdot (k + 1)
r 2 ⋅ d 2 R ( r ) d r 2 \displaystyle r^2 \cdot \frac{\displaystyle d^2 R(r)}{\displaystyle dr^2} + 2 ⋅ r ⋅ d R ( r ) d r \displaystyle + 2 \cdot r \cdot \frac{\displaystyle d R(r)}{\displaystyle dr} + ( r 2 ⋅ γ 2 − k ⋅ ( 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 R ( r ) \displaystyle R(r) = 1 r ⋅ J k + 1 / 2 ( γ ⋅ r ) , \displaystyle = \frac{\displaystyle 1}{\displaystyle \sqrt r} \cdot J_{k + 1/2}(\gamma \cdot r), ). It should be noted that the solution is bounded at the point r r = 0 = 0 : the Bessel function J k + 1 / 2 ( γ ⋅ r ) J_{k + 1/2}(\gamma \cdot r) tends to zero no slower than r \sqrt{r} .
Thus, the solutions of equation (2.76 ∂ 2 Ψ ( r , θ , ϕ ) ∂ r 2 \displaystyle \frac{\displaystyle \partial^2 \Psi(r, \theta, \phi)}{\displaystyle \partial r^2} + 2 r ⋅ ∂ Ψ ( r , θ , ϕ ) ∂ r \displaystyle + \frac{\displaystyle 2}{\displaystyle r} \cdot \frac{\displaystyle \partial \Psi(r, \theta, \phi)}{\displaystyle \partial r} + 1 r 2 ⋅ sin ( 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) + 1 r 2 ⋅ sin 2 θ ⋅ ∂ 2 Ψ ( r , θ , ϕ ) ∂ ϕ 2 \displaystyle + \frac{\displaystyle 1}{\displaystyle r^2 \cdot \sin^2 \theta} \cdot \frac{\displaystyle \partial^2 \Psi(r, \theta, \phi)}{\displaystyle \partial \phi^2} + γ 2 ⋅ Ψ ( r , θ , ϕ ) \displaystyle + \gamma^2 \cdot \Psi(r, \theta, \phi) = 0. \displaystyle = 0. ) have the form
Let us substitute the solutions (2.82 Ψ 1 k m ( r , θ , ϕ ) = A k m ⋅ 1 r ⋅ J k + 1 / 2 ( γ ⋅ r ) ⋅ P k ( m ) ( cos ( θ ) ) ⋅ sin ( m ⋅ ϕ ) , 1 ≤ m ≤ k , k ≥ 1 , \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} Ψ 2 k m ( r , θ , ϕ ) = A k m ⋅ 1 r ⋅ J k + 1 / 2 ( γ ⋅ r ) ⋅ P k ( m ) ( cos ( θ ) ) ⋅ cos ( m ⋅ ϕ ) , 0 ≤ m ≤ k , k ≥ 0 , \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} ) into the boundary conditions (2.73 ∂ T ^ ( r , θ , ϕ , t ) ∂ t \displaystyle \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial t} = a 2 ⋅ ∂ 2 T ^ ( r , θ , ϕ , t ) ∂ r 2 \displaystyle = a^2 \cdot \frac{\displaystyle \partial^2 \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial r^2} + 2 ⋅ a 2 r ⋅ ∂ T ^ ( 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} + a 2 r 2 ⋅ sin ( 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) + a 2 r 2 ⋅ sin 2 θ ⋅ ∂ 2 T ^ ( r , θ , ϕ , t ) ∂ ϕ 2 \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) = T 0 ( 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 + 2 π , t ) , \displaystyle = \widehat{T}(r, \theta, \phi + 2\pi, t), ) and obtain
A k m ⋅ 1 R ⋅ J k + 1 / 2 ( γ ⋅ R ) ⋅ P k ( m ) ( cos ( θ ) ) ⋅ sin ( m ⋅ ϕ ) \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, A k m ⋅ 1 R ⋅ J k + 1 / 2 ( γ ⋅ R ) ⋅ P k ( m ) ( cos ( θ ) ) ⋅ cos ( m ⋅ ϕ ) \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 A k m A_{km} ≠ 0 \neq 0 , which is possible only when J k + 1 / 2 ( γ ⋅ R ) J_{k + 1/2}(\gamma \cdot R) = 0 = 0 . Let us denote the roots of the equation J k + 1 / 2 ( μ ) J_{k + 1/2}(\mu) = 0 = 0 by μ k s \mu_{ks} — then the eigenvalues take the form
Zero and negative roots are no good: for μ \mu = 0 = 0 the eigenfunction J k + 1 / 2 ( 0 ⋅ r ) J_{k + 1/2}(0 \cdot r) ≡ 0 \equiv 0 — identically zero, which is not an eigenfunction (the index k k + 1 / 2 + 1/2 > 0 > 0 ), and negative roots give no new solutions. Therefore we take only the positive roots: μ k s , s \mu_{ks}, s ∈ ( 1.. ∞ ) \in (1..\infty) .
Thus, the eigenvalues and eigenfunctions have the form
where A k m s A_{kms} is an arbitrary constant factor: the eigenfunction is defined up to it. Let us set A k m s A_{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 Ψ 1 k m s ( r , θ , ϕ ) \Psi_{1kms}(r, \theta, \phi) and Ψ 2 k m s ( r , θ , ϕ ) \Psi_{2kms}(r, \theta, \phi) we need to compute the norms ∥ Ψ 1 k m s ( r , θ , ϕ ) ∥ 2 \|\Psi_{1kms}(r, \theta, \phi)\|^2 and ∥ Ψ 2 k m s ( r , θ , ϕ ) ∥ 2 \|\Psi_{2kms}(r, \theta, \phi)\|^2 ; the weight for spherical coordinates is ρ ( r , θ , ϕ ) \rho(r, \theta, \phi) = r 2 ⋅ sin ( θ ) = r^2 \cdot \sin(\theta) .
∥ Ψ 1 k m s ∥ 2 \displaystyle \|\Psi_{1kms}\|^2 = ∫ 0 R r ⋅ J k + 1 / 2 2 ( γ k s ⋅ r ) d r ∫ 0 π [ P k ( m ) ( cos θ ) ] 2 sin ( θ ) d θ ⋅ ⋅ ∫ 0 2 π sin 2 ( m ϕ ) d ϕ , 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, ∥ Ψ 2 k m s ∥ 2 \displaystyle \|\Psi_{2kms}\|^2 = ∫ 0 R r ⋅ J k + 1 / 2 2 ( γ k s ⋅ r ) d r ∫ 0 π [ P k ( m ) ( cos θ ) ] 2 sin ( θ ) d θ ⋅ ⋅ ∫ 0 2 π cos 2 ( m ϕ ) d ϕ , 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 ∫ 0 2 π sin 2 ( m ⋅ θ ) d θ \displaystyle \int_0^{2\pi} \sin^2(m \cdot \theta) \,d\theta = π , m \displaystyle = \pi, m ∈ ( 1.. ∞ ) , \displaystyle \in (1..\infty), ∫ 0 2 π cos 2 ( m ⋅ θ ) d θ \displaystyle \int_0^{2\pi} \cos^2(m \cdot \theta) \,d\theta = { 2 ⋅ π , m = 0 , π , m ≥ 1 , m \displaystyle = \begin{cases} 2 \cdot \pi, & m = 0, \\ \pi, & m \geq 1 \end{cases}, m ∈ ( 0.. ∞ ) . \displaystyle \in (0..\infty). ), the integral over the radius is the same as in the Dirichlet problem for the disk: after the substitution x x = γ k s ⋅ r = \gamma_{ks} \cdot r it is evaluated by formula (C.6 ∫ 0 μ r ⋅ J m 2 ( r ) d r \displaystyle \int_0^{\mu} r \cdot J_m^2(r) \,dr = μ 2 2 ⋅ J m + 1 2 ( μ ) . \displaystyle = \frac{\displaystyle \mu^2}{\displaystyle 2} \cdot J_{m+1}^2(\mu). ), and the integral over the angle θ \theta after the substitution z z = cos ( θ ) = \cos(\theta) is exactly the norm of the associated Legendre polynomial (F.6 ∫ − 1 1 [ P k ( m ) ( z ) ] 2 d z \displaystyle \int_{-1}^1 \left[ P_k^{(m)}(z) \right]^2 \,dz = 2 2 ⋅ k + 1 ⋅ ( k + m ) ! ( k − m ) ! , m \displaystyle = \frac{\displaystyle 2}{\displaystyle 2 \cdot k + 1} \cdot \frac{\displaystyle (k+m)!}{\displaystyle (k-m)!}, \quad m ≤ k . \displaystyle \leq k. ). Let us put it all together
Now let us substitute the solution (2.82 Ψ 1 k m ( r , θ , ϕ ) = A k m ⋅ 1 r ⋅ J k + 1 / 2 ( γ ⋅ r ) ⋅ P k ( m ) ( cos ( θ ) ) ⋅ sin ( m ⋅ ϕ ) , 1 ≤ m ≤ k , k ≥ 1 , \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} Ψ 2 k m ( r , θ , ϕ ) = A k m ⋅ 1 r ⋅ J k + 1 / 2 ( γ ⋅ r ) ⋅ P k ( m ) ( cos ( θ ) ) ⋅ cos ( m ⋅ ϕ ) , 0 ≤ m ≤ k , k ≥ 0 , \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} ) into the boundary conditions (2.75 ∂ T ^ ( r , θ , ϕ , t ) ∂ t \displaystyle \frac{\displaystyle \partial \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial t} = a 2 ⋅ ∂ 2 T ^ ( r , θ , ϕ , t ) ∂ r 2 \displaystyle = a^2 \cdot \frac{\displaystyle \partial^2 \widehat{T}(r, \theta, \phi, t)}{\displaystyle \partial r^2} + 2 ⋅ a 2 r ⋅ ∂ T ^ ( 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} + a 2 r 2 ⋅ sin ( 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) + a 2 r 2 ⋅ sin 2 θ ⋅ ∂ 2 T ^ ( r , θ , ϕ , t ) ∂ ϕ 2 \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) = T 0 ( 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 ) ∂ n ∣ r = 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 + 2 π , t ) , \displaystyle = \widehat{T}(r, \theta, \phi + 2\pi, t), ); since the direction of the normal coincides with the direction of the coordinate r r , we obtain
A k m ⋅ [ − 1 2 ⋅ R ⋅ R ⋅ J k + 1 / 2 ( γ ⋅ R ) + γ R ⋅ J k + 1 / 2 ′ ( γ ⋅ R ) ] ⋅ P k ( m ) ( cos ( θ ) ) ⋅ sin ( m ⋅ ϕ ) = 0 , 1 ≤ m ≤ k , k ≥ 1 , \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} A k m ⋅ [ − 1 2 ⋅ R ⋅ R ⋅ J k + 1 / 2 ( γ ⋅ R ) + γ R ⋅ J k + 1 / 2 ′ ( γ ⋅ R ) ] ⋅ P k ( m ) ( cos ( θ ) ) ⋅ cos ( m ⋅ ϕ ) = 0 , 0 ≤ m ≤ k , k ≥ 0 , \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 A k m A_{km} ≠ 0 \neq 0 , which is possible only when γ ⋅ J k + 1 / 2 ′ ( γ ⋅ R ) \gamma \cdot J_{k + 1/2}'(\gamma \cdot R) = 1 2 ⋅ R ⋅ J k + 1 / 2 ( γ ⋅ R ) = \frac{\displaystyle 1}{\displaystyle 2 \cdot R} \cdot J_{k + 1/2}(\gamma \cdot R) . Let us denote the roots of the equation J k + 1 / 2 ′ ( μ ) J_{k + 1/2}'(\mu) = 1 2 ⋅ μ ⋅ J k + 1 / 2 ( μ ) = \frac{\displaystyle 1}{\displaystyle 2 \cdot \mu} \cdot J_{k + 1/2}(\mu) by μ k s \mu_{ks} — then the eigenvalues take the form
Here, unlike the Dirichlet problem, the zero mode survives: for k k = 0 = 0 the radial solution is the spherical Bessel function j 0 ( γ ⋅ r ) j_0(\gamma \cdot r) = sin ( γ ⋅ r ) γ ⋅ r = \frac{\displaystyle \sin(\gamma \cdot r)}{\displaystyle \gamma \cdot r} , and zero is a root of the Neumann condition (j 0 ′ ( 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: μ 01 \mu_{01} = 0 = 0 . For k k ≥ 1 \geq 1 the zero root gives no eigenfunction (j k ( 0 ) j_k(0) = 0 = 0 ), so there we still take only the positive roots.
Thus, the eigenvalues and eigenfunctions have the form
where A k m s A_{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 ∫ 0 μ r ⋅ J k + 1 / 2 2 ( r ) d r \displaystyle \int_0^{\mu} r \cdot J_{k+1/2}^2(r) \,dr = μ 2 − k ⋅ ( k + 1 ) 2 ⋅ J k + 1 / 2 2 ( μ ) . \displaystyle = \frac{\displaystyle \mu^2 - k \cdot (k+1)}{\displaystyle 2} \cdot J_{k+1/2}^2(\mu). ) to compute the norm
∫ 0 R r ⋅ J k + 1 / 2 2 ( γ k s ⋅ r ) d r \displaystyle \int_0^{R} r \cdot J_{k + 1/2}^2(\gamma_{ks} \cdot r) \,dr = R 2 2 ⋅ [ 1 − k ⋅ ( k + 1 ) μ k s 2 ] ⋅ J k + 1 / 2 2 ( μ k s ) . \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 μ 01 \mu_{01} = 0 = 0 (for γ 01 \gamma_{01} = 0 = 0 the eigenfunction Ψ 2001 ( r , θ , ϕ ) \Psi_{2001}(r, \theta, \phi) = 1 = 1 ) we compute separately
The norms ∥ Ψ 1 k m s ( r , θ , ϕ ) ∥ 2 \|\Psi_{1kms}(r, \theta, \phi)\|^2 and ∥ Ψ 2 k m s ( r , θ , ϕ ) ∥ 2 \|\Psi_{2kms}(r, \theta, \phi)\|^2 have the form
The final solution of the three-dimensional Dirichlet boundary value problem with inhomogeneous boundary conditions takes the form
In the Neumann problem, unlike the Dirichlet one, the spectrum contains the zero mode (γ 01 \gamma_{01} = 0 = 0 , Ψ 2001 ( r , θ , ϕ ) \Psi_{2001}(r, \theta, \phi) = 1 = 1 ) — the case γ \gamma = 0 = 0 , which in the general solution (2.18 T ( M ) \displaystyle T(M) = ∑ n = 1 ∞ Ψ n ( M ) ∥ Ψ n ( M ) ∥ 2 ⋅ 1 a 2 ⋅ γ n 2 ⋅ ∭ G ρ ( M ) ⋅ f ( M ) ⋅ Ψ n ( M ) d G , γ n \displaystyle = \sum_{n=1}^{\infty} \frac{\displaystyle \Psi_n(M)}{\displaystyle \|\Psi_n(M)\|^2} \cdot \frac{\displaystyle 1}{\displaystyle a^2 \cdot \gamma_n^2} \cdot \iiint_G \rho(M) \cdot f(M) \cdot \Psi_n(M) \,dG, \quad \gamma_n ≠ 0. \displaystyle \neq 0. ) was set aside for separate consideration; it is precisely what gives the non-decaying term — the term with k k = 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
To obtain the stationary solutions, we let time tend to infinity in the solutions found (t t → ∞ \to \infty ), as was done for the general case in (2.18 T ( M ) \displaystyle T(M) = ∑ n = 1 ∞ Ψ n ( M ) ∥ Ψ n ( M ) ∥ 2 ⋅ 1 a 2 ⋅ γ n 2 ⋅ ∭ G ρ ( M ) ⋅ f ( M ) ⋅ Ψ n ( M ) d G , γ n \displaystyle = \sum_{n=1}^{\infty} \frac{\displaystyle \Psi_n(M)}{\displaystyle \|\Psi_n(M)\|^2} \cdot \frac{\displaystyle 1}{\displaystyle a^2 \cdot \gamma_n^2} \cdot \iiint_G \rho(M) \cdot f(M) \cdot \Psi_n(M) \,dG, \quad \gamma_n ≠ 0. \displaystyle \neq 0. ). The term with the initial condition vanishes, since e − a 2 ⋅ γ k s 2 ⋅ t e^{- 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 γ k s \gamma_{ks} ≠ 0 \neq 0 gives the factor 1 a 2 ⋅ γ k s 2 \frac{1}{a^2 \cdot \gamma_{ks}^2} :
∫ 0 t e − a 2 ⋅ γ k s 2 ⋅ ( t − τ ) d τ \displaystyle \int_0^t e^{- a^2 \cdot \gamma_{ks}^2 \cdot (t - \tau)} \,d\tau = 1 a 2 ⋅ γ k s 2 ⋅ ( 1 − e − a 2 ⋅ γ k s 2 ⋅ t ) \displaystyle = \frac{\displaystyle 1}{\displaystyle a^2 \cdot \gamma_{ks}^2} \cdot (1 - e^{- a^2 \cdot \gamma_{ks}^2 \cdot t}) → 1 a 2 ⋅ γ k s 2 as t \displaystyle \rightarrow \frac{\displaystyle 1}{\displaystyle a^2 \cdot \gamma_{ks}^2} \quad \text{as} \quad t → ∞ , γ k s \displaystyle \rightarrow \infty, \quad \gamma_{ks} ≠ 0. \displaystyle \neq 0. The stationary solution of the three-dimensional Dirichlet boundary value problem takes the form
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 a 2 ⋅ Δ T ^ ( 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 = ∫ 0 R ∫ 0 π ∫ 0 2 π ( a 2 ⋅ Δ T ^ + f ^ ) ⋅ r 2 ⋅ sin ( θ ) d r d θ d ϕ = a 2 ⋅ ∮ r = R ∂ T ^ ∂ n d S + ∫ 0 R ∫ 0 π ∫ 0 2 π f ^ ⋅ r 2 ⋅ sin ( θ ) d r d θ d ϕ = ∫ 0 R ∫ 0 π ∫ 0 2 π f ^ ⋅ r 2 ⋅ sin ( θ ) d r d θ d ϕ . \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 ∭ G f ( M ) d M \displaystyle \iiint_G f(M) \,dM = − a 2 ⋅ ∬ S Φ ( M ) d S , \displaystyle = - a^2 \cdot \iint_S \Phi(M) \,dS, ): ∫ 0 R ∫ 0 π ∫ 0 2 π f ^ ( r , θ , ϕ ) ⋅ r 2 ⋅ sin ( θ ) d r d θ d ϕ \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 C C : it corresponds to the zero mode (γ 01 \gamma_{01} = 0 = 0 , Ψ 2001 ( 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
Two-dimensional heat conduction boundary value problem Storage formats