Boundary conditions. Diffusion 2: Boundary conditions, long time behavior

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Boundary conditions In a domain Ω one has to add boundary conditions to the heat (or diffusion) equation: 1. u(x, t) = φ for x Ω. Temperature given at the boundary. Also density given at the boundary. (Dirichlet) 2. ku n (x, t) = φ for x Ω. Flux given at the boundary. The most typical is φ 0, isolated boundaries. (Neumann) 3. ku n (x, t) + hu(x, t) = φ for x Ω. These are called convection boundary conditions in the thermal engineering literature: k u n = h(u u ) if the temperature of the fluid around the body is u far away. (third class, Robin, convection, Newton) 4. Perfect thermal contact: k 1 u 1 n = k 2 u 2 n. (n is the exterior unit normal to Ω 1 ).

5. Dynamic boundary conditions: u t + αu n = φ at the boundary. Example: bar ( 1 < x < 1) with ends immersed into two fluid containers, at homogeneous temperatures a(t) and b(t). d V f C f ρ f dt a(t) = ku n ds = Aku x ( 1, t) A V f C f ρ f d dt b(t) = Aku x(1, t) a (t) = αu x, b (t) = αu x, u( 1, t) = a(t) and u(1, t) = b(t). So, u t ( 1, t) + α( u x ( 1, t)) = 0 and u t (1, t) + αu x (1, t) = 0.

Example: (to understand conductivity, or diffusivity) Calculate the steady-state temperature profiles inside a wall 1 < x < 1 made of two parts in perfect thermal contact: one is 1 < x < 0 with conductivity k and the other is 0 < x < 1 of conductivity 1. The boundary temperatures are u = 0 for x = 1 and u = 1 for x = 1. u xx = 0, for 1 < x < 0 and 0 < x < 1, u( 1) = 0, u(0 ) = u(0 + ), ku x (0 ) = u x (0 + ) u(1) = 1. The solution is u = (x + 1)/(1 + k) for 1 < x < 0 and u = (kx + 1)/(1 + k) for 0 < x < 1.

Problem 3.1: (lumped approximation) Calculate the steady-state temperature profiles inside a wall 1 < x < 1 made of three parts in perfect thermal contact: one is 1 < x < ε with conductivity 1, the second is ε < x < ε with conductivity k (small) and the third is ε < x < 1 with conductivity 1. The boundary temperatures are u = a for x = 1 and u = b for x = 1. Observe that for k small, u a in the first part and u b in the third part. How small (with ε) should k be to keep this property as ε 0?

Dissipation and limit behavior (bounded domain) Imagine u = 0 and the three cases of boundary values for u t = D 2 u: (1) u = 0; (2) u n = (h/k)u, with h > 0; and (3) u n = 0. One has d dt Ω 1 2 u2 = D ( u) 2 + D uu n. Ω Ω In cases (1) and (2) this is strictly negative, unless u 0. In case (3) this is strictly negative, unless u constant. Also, d 1 dt 2 ( u)2 = D ut 2 + D u t u n. Ω In cases (1) and (3) this is strictly negative, except at equilibria. In case (2) we have d ( 1 dt Ω 2 ( u)2 + (Dh/k) 1 Ω 2 u2) is strictly negative, except at equilibria. Ω Ω

Problem 3.2: By showing that 1 2 u2 tends exponentially to zero, show that all solutions of u t = D 2 u with u = 0 at Ω tend to zero exponentially, provided that Ω is bounded in one direction, that is Ω {a < x i < a + L}. Hint: show first Poincaré s inequality. If Ω is bounded in some direction and u(x) is a smooth function in Ω that vanishes at Ω, then there exists a constant C > 0, independent of u such that Ω u2 C Ω ( u)2. Can one show, with similar methods, that all the solutions of u t = D 2 u with u n = 0 at Ω tend exponentially to a steady solution? Given the initial condition u(x, 0) can one predict which is the value of the constant solution at which u(x, t) tends as t?

Dissipation and limit behavior (infinite domain) Dimension one, k = 1. Non-negative solutions with finite mass: 0 u(x, 0), u(, 0 1 <. 0 u(x, t) 1 4πt u(, 0) 1. Also, we have the particular solutions G(x, t) = (4πt) 1/2 e x 2 /(4t). So, t 1/2 is the optimal power. Problem 3.3: Suppose 0 u(x, 0), u(, 0) 1 <, and u(x, 0) nonzero. Prove that there is a value x 0 and a constant C > 0 such that u(x 0, t) C/ t for t sufficiently large. For large t every positive solution approaches a Gaussian: Suppose 0 u(x, 0) M 1 (1 + x 2 ) α for some α > 1, and that u(, 0) 1 = M 2. Then it can be proved that u(, t) M 2 G(, t) 1/t.

Entropy If an event happens with probability p, its (Shannon) amount of information is log p. If there are n possible events, with probabilities p i, the (Shannon) entropy H of the system is the expected value of the amount of information: p i log p i (> 0). If we have a pdf u(x) for < x < and a partition {ih x < (i + 1)x, k Z} the entropy would be ( ) ( (i+1)h ) (i+1)h u dx log u dx i ih u(ih)h log(u(ih)h) log h i ih u log u dx and we define its (renormalized) entropy as h[u] = u log u dx. Observe that needs not to be positive.

If u satisfies u t = u xx then d dt h[u] = u xx log u u xx }{{} =0 ( ) = (u x log u) x + u x 2 /u = u x 2 /u > 0, so the entropy always increases. The same is true in n dimensions or in a bounded domain with Neumann boundary conditions. Also, for the gaussian G log G = ( 1 e x2 4t log 4πt 1 x 2 ) 4πt 4t Problem 3.4: Show that the first term tends to infinity as log t and the second does not depend on t.

α 0 = 1 a Separation of variables in an interval a 0 u t = u xx u(x, t) = in 0 < x < a u x (0) = u x (a) = 0 n=0 u(x, 0) dx, α n = 2 a π2 n2 α n e a 2 t cos n π a x a 0 u(x, 0) cos nπ a x dx.

Separation of variables in a rectangle u t = 2 u in 0 < x < a, 0 < y < b with Neumann boundary conditions. u(x, y, t) = n,m 1=0 n,m=0 α nm e n=0 π2 π2 (n2 a2 +m2 π2 n2 α n0 e a 2 t cos(n π a x)+ π2 π2 (n2 2 +m2 b 2 )t α nm e a }{{} e π2 t/b 2 b 2 )t cos(n π a x) cos(m π b y) = π cos(n a x) cos(m π b y). So, if 0 < b 1 u becomes shortly independent of y and satisfies simply u t = u xx in 0 < x < a with Neumann boundary conditions.

Thin (slender) domains Ω ε = {(x, y) 0 < x < a, 0 < y < εg(x)}, u t = D 2 u in Ω ε, u/ n = 0 on Ω ε. Suppose u(x, y, t) = u 0 (x, t) + εu 1 (x, y, t) + O(ε 2 ), and the same for the x-derivatives. d dt x2 εg(x) x 1 0 u(x, y, t) dy dx = εg(x2 ) 0 Du x dy εg(x1 ) 0 Du x dy d x2 εg(x)u 0 (x, t) dx = εg(x 2 )Dux 0 (x 2, t) εg(x 1 )Du x (x 1, t) dt x 1 x2 x 1 g(x)u 0 t (x, t) dx = x2 x 1 (g(x)du 0 x (x, t)) x dx u 0 t = D g(x) (g(x)u0 x ) x, u 0 t = Du 0 xx + D g (x) g(x) u0 x.