Symbolic Computation of Conservation Laws of Nonlinear Partial Differential Equations Willy Hereman Department of Mathematical and Computer Sciences Colorado School of Mines Golden, Colorado, U.S.A. whereman@mines.edu http://inside.mines.edu/∼whereman/ Universidad Nacional de Ingenierı́a Lima, Peru Friday, March 13, 2009, 2:00p.m. . Acknowledgements Loren ‘Douglas’ Poole Ph.D. student, CSM Research supported in part by NSF under Grant CCF-0830783 This presentation was made in TeXpower . In Memory of Martin D. Kruskal (1925-2006) . Outline • Conservation laws of nonlinear PDEs • Famous examples in historical perspective • Example: Shallow water wave equations (Dellar) • Algorithmic method for conservation laws • Computer demonstration • Tools: • The variational derivative (testing exactness) • The homotopy operator (inverting Dx and Div) • Application to shallow water wave equations • Additional examples • Conclusions and future work . Conservation Laws • Conservation law in (1+1)-dimensions Dt ρ + Dx J = 0 (on PDE) conserved density ρ and flux J • Conservation law in (3+1)-dimensions Dt ρ + ∇ · J = Dt ρ + Dx J1 + Dy J2 + Dz J3 = 0 (on PDE) conserved density ρ and flux J = (J1 , J2 , J3 ) . Famous Examples in Historical Perspective • Example: Korteweg-de Vries (KdV) equation ∂u ∂u ∂3u +u + =0 3 ∂t ∂x ∂x Diederik Korteweg Gustav de Vries • First six (of ∞ many) densities-flux pairs: ! u2 Dt (u) + Dx + u2x = 0 2 2 3 2 Dt u + D x u − ux 2 + 2uu2x = 0 3 Dt u3 − 3ux 2 + 3 4 u − 6uux 2 + 3u2 u2x + 3u2x 2 − 6ux u3x = 0 Dx 4 108 2 5 2 2 2 u3x + Dt u − 30 u ux + 36 uu2x − 7 5 6 216 3 2 Dx u − 40u ux − . . . − u3x u5x = 0 6 7 Dt u6 − 60 u3 ux 2 − 30 ux 4 + 108 u2 u2x 2 648 216 720 3 2 u2x − uu3x + u4x 2 + + 7 7 7 6 7 432 4 2 Dx u − 75u ux − . . . + u4x u6x = 0 7 7 • Third conservation law: Gerald Whitham, 1965 • Fourth and fifth: Norman Zabusky, 1965-66 • Sixth: algebraic mistake, 1966 • Seventh (sixth thru tenth): Robert Miura, 1966 . Robert Miura . • First five: IBM 7094 computer with FORMAC (1966) — storage space problem! • First eleven densities: AEC CDC-6600 computer (2.2 seconds) — large integers problem! • 2006 Leroy P. Steele Prize (AMS): Gardner, Greene, Kruskal, and Miura • National Medal of Science, von Neuman Prize (SIAM), . . .: Martin Kruskal . • Key property: Dilation invariance • Example: KdV equation and its density-flux pairs are invariant under the scaling symmetry x t (x, t, u) → ( , 3 , λ2 u) λ λ λ is arbitrary parameter • Examples of conservation laws 2 3 2 Dt u + D x u − ux 2 + 2uu2x = 0 3 Dt u3 − 3ux 2 + 3 4 Dx u − 6uux 2 + 3u2 u2x + 3u2x 2 − 6ux u3x = 0 4 . Transcendental Equations in (1+1)-Dimensions • Example: sine-Gordon equation UXT = sin U or utt − uxx = sin u Written as a first order system: ut = v vt = uxx + α sin u • Scaling invariance (trick!) x t 0 (x, t, u, v, α) → ( , , λ u, λv, λ2 α) λ λ λ is arbitrary parameter • . First few densities-flux pairs ρ(1) = 2α cos u + v 2 + ux 2 ρ(2) = 2ux v J(1) = −2ux v J(2) = 2α cos u − v 2 − ux 2 ρ(3) = 12vux cos u + 2v 3 ux + 2vux 3 − 16vx u2x ρ(4) = 2 cos2 u − 2 sin2 u + v 4 + 6v 2 ux 2 + ux 4 + 4v 2 cos u + 20ux 2 cos u − 16vx 2 − 16u2x 2 J(3) and J(4) are not shown (too long) . An Example in (2+1)-Dimensions • Example: Shallow water wave (SWW) equations [P. Dellar, Phys. Fluids 15 (2003) 292-297] 1 ut + (u·∇)u + 2 Ω × u + ∇(θh) − h∇θ = 0 2 θt + u·(∇θ) = 0 ht + ∇·(uh) = 0 where u(x, y, t), θ(x, y, t) and h(x, y, t) . • In components: 1 ut + uux + vuy − 2 Ωv + hθx + θhx = 0 2 1 vt + uvx + vvy + 2 Ωu + hθy + θhy = 0 2 θt + uθx + vθy = 0 ht + hux + uhx + hvy + vhy = 0 • SWW equations are invariant under (x, y, t, u, v, h, θ, Ω) → (λ−1 x, λ−1 y, λ−b t, λb−1 u, λb−1 v, λa h, λ2b−a−2 θ, λb Ω) where W (h) = a and W (Ω) = b (a, b ∈ Q) • First few densities-flux pairs of SWW system: uh (1) ρ(1) = h J = vh uhθ (2) ρ(2) = hθ J = vhθ 2 uhθ ρ(3) = hθ2 J(3) = vhθ2 3 h + uv 2 h + 2uh2 θ u ρ(4) = (u2 + v 2 )h + h2 θ J(4) = v 3 h + u2 vh + 2vh2 θ ρ(5) = (2Ω + vx − uy )θ (4Ωu − 2uuy + 2uvx − hθy )θ 1 (5) J =2 (4Ωv + 2vvx − 2vuy + hθx )θ Generalizations: Dt (f (θ)h) + Dx (f (θ)uh) + Dy (f (θ)vh) = 0 Dt g(θ)(2Ω + vx − ux ) 1 g(θ)(4Ωu − 2uuy + 2uvx − hθy ) + Dx 2 1 + Dy g(θ)(4Ωv − 2uy v + 2vvx + hθx ) = 0 2 for any functions f (θ) and g(θ) . Reasons to Compute Conservation Laws I Conservation of physical quantities (linear momentum, mass, energy) I Verify the closure of a model I Testing of complete integrability and application of Inverse Scattering Transform I Testing of numerical integrators I Study of quantitative and qualitative properties of PDEs (Hamiltonian structure, recursion operators) Notation – Computations on the Jet Space I Independent variables x = (x, y, z) I Dependent variables u = (u(1) , u(2) , . . . , u(j) , . . . , u(N ) ) In examples: u = (u, v, θ, h, . . .) ∂k u , ∂xk I Partial derivatives ukx = I Differential functions Example: f = uvvx + x2 u3x vx + ux vxx Total derivative (with respect to x) I ukx ly = (1) ∂ Dx = + ∂x (1) Mx M x X k=0 ∂ k+l u , ∂xk y l etc. (2) ∂ u(k+1)x + ∂ukx M x X k=0 ∂ v(k+1)x ∂vkx is the order of f in u (with respect to x) . I Example: f = uvvx + x2 u3x vx + ux vxx (1) (2) Here, Mx = 1 and Mx = 2 I Total derivative with respect to x: 1 2 X X ∂f ∂f ∂f + v(k+1)x + u(k+1)x Dx f = ∂x k=0 ∂ukx k=0 ∂vkx ∂f ∂f ∂f = + ux + u2x ∂x ∂u ∂ux ∂f ∂f ∂f +vx + v2x + v3x ∂v ∂vx ∂v2x = 2xu3x vx + ux (vvx ) + uxx (3x2 u2x vx + vxx ) +vx (uvx ) + vxx (uv + x2 u3x ) + vxxx (ux ) . A Method to Compute Conservation Laws I Density is linear combination of scaling invariant terms with undetermined coefficients I Compute Dt ρ with total derivative operator I Use variational derivative (Euler operator) to compute the undetermined coefficients I Use homotopy operator to compute flux J (invert Dx or Div) I Use linear algebra and variational calculus (algorithmic) I Work with linearly independent pieces in finite dimensional spaces . Algorithm for PDEs in (1+1)-dimensions I Example: Density of rank 6 for the KdV equation ut + uux + u3x = 0 I Step 1: Compute the dilation symmetry Set W (Dx ) = 1 and solve W (u) + W (Dt ) = 2W (u) + 1 = W (u) + 3 Hence, W (u) = 2, W (Dt ) = 3 Thus, x t (x, t, u) → ( , 3 , λ2 u) λ λ . I Step 2: Determine the form of the density List powers of u, up to rank 6 : [u, u2 , u3 ] Introduce x derivatives to ‘adjust’ the rank u has weight 2, introduce D4x u2 has weight 4, introduce D2x u3 has weight 6, no derivative needed . Apply the Dx derivatives Remove total and highest derivative terms: [u4x ] → [ ] [ux 2 , uu2x ] → [ux 2 ] empty list since uu2x = (uux )x − ux 2 [u3 ] → [u3 ] Linearly combine the “building blocks” Candidate density: ρ = c1 u3 + c2 ux 2 . I Step 3: Compute the coefficients ci Compute ∂ρ Dt ρ = + ρ0 (u)[ut ] ∂t M X ∂ρ ∂ρ k Dx ut = + ∂t ∂u kx k=0 = (3c1 u2 I + 2c2 ux Dx )ut Substitute ut by −(uux + u3x ) E = −Dt ρ = (3c1 u2 I + 2c2 ux Dx )(uux + u3x ) = 3c1 u3 ux + 2c2 u3x + 2c2 uux u2x +3 c1 u2 u3x + 2c2 ux u4x . Apply the Euler operator (variational derivative) m X (0) k ∂ Lu = (−Dx ) ∂ukx k=0 Here, E has order m = 4, thus L(0) u E ∂E ∂E 2 ∂E 3 ∂E 4 ∂E = − Dx + Dx − Dx + Dx ∂u ∂ux ∂u2x ∂u3x ∂u4x = −6(3c1 + c2 )ux u2x This term must vanish! So, c1 = − 31 c2 . Set c2 = −3, then c1 = 1 Hence, the final form density is ρ = u3 − 3ux 2 . I Step 4: Compute the flux J Method 1: Integrate by parts (simple cases) Now, E = 3u3 ux + 3u2 u3x − 6u3x − 6uux u2x − 6ux u4x Integration of Dx J = E yields final form of the flux 3 4 J = u − 6uux 2 + 3u2 u2x + 3u2x 2 − 6ux u3x 4 . Method 2: Build the form of J (cumbersome) Note: Rank J = Rank ρ + Rank Dt − 1 Build up form of J. Compute m X ∂J ∂J u(k+1)x Dx J = + ∂x k=0 ∂ukx m is the order of J. Match Dx J = E . Method 3: Use the homotopy operator (most powerful) Z Z 1 dλ −1 (Iu E)[λu] J = Dx E = E dx = Hu(x) E = λ 0 with integrand M k−1 X X k−(i+1) ∂E Iu E = uix (−Dx ) ∂ukx i=0 k=1 Here M = 4, thus ∂E ∂E Iu E = (uI)( ) + (ux I − uDx )( ) ∂ux ∂u2x ∂E 2 +(u2x I − ux Dx + uDx )( ) ∂u3x +(u3x I − u2x Dx + ux D2x − uD3x )( ∂E ) ∂u4x = (uI)(3u3 + 18u2x − 6uu2x − 6u4x ) +(ux I − uDx )(−6uux ) +(u2x I − ux Dx + uD2x )(3u2 ) +(u3x I − u2x Dx + ux D2x − uD3x )(−6ux ) = 3u4 − 18uu2x + 9u2 u2x + 6u22x − 12ux u3x Note: correct terms but incorrect coefficients! Finally, Z J = Hu(x) E = 0 = Z 1 1 dλ (Iu E)[λu] λ 3λ3 u4 − 18λ2 uu2x + 9λ2 u2 u2x + 6λu22x 0 −12λux u3x ) dλ 3 4 = u − 6uu2x + 3u2 u2x + 3u22x − 6ux u3x 4 Final form of the flux: 3 4 J = u − 6uux 2 + 3u2 u2x + 3u2x 2 − 6ux u3x 4 . Computer Demonstration . I Review of Vector Calculus Definition: F is conservative if F = ∇f I Definition: F is irrotational or curl free if ∇×F=0 I Theorem: F = ∇f iff ∇ × F = 0 The curl annihilates gradients! I Definition: F is incompressible or divergence free if ∇ · F = 0 Theorem: F = ∇ × G iff ∇ · F = 0 The divergence annihilates curls! Question: How can one test that f = ∇ · F ? I . I Review of Vector Calculus Definition: F is conservative if F = ∇f I Definition: F is irrotational or curl free if ∇×F=0 I Theorem: F = ∇f iff ∇ × F = 0 The curl annihilates gradients! I Definition: F is incompressible or divergence free if ∇ · F = 0 Theorem: F = ∇ × G iff ∇ · F = 0 The divergence annihilates curls! Question: How can one test that f = ∇ · F ? No theorem from vector calculus! I . I Tools from the Calculus of Variations Definition: A differential function f is exact iff f = Dx F I Theorem (exactness test): (0) f = Dx F iff Lu(j) (x) f ≡ 0, j = 1, 2, . . . , N I Definition: A differential function f is a divergence if f = Div F I Theorem (exactness test): (0) f = Div F iff Lu(j) (x) f ≡ 0, j = 1, 2, . . . , N The Euler operator annihilates divergences! . Formula for Euler operator in 1D: (j) (0) Lu(j) (x) = M x X (−Dx ) k k=0 ∂ (j) ∂ukx ∂ ∂ 2 ∂ 3 ∂ = − Dx (j) + Dx (j) − Dx (j) + · · · (j) ∂u ∂ux ∂u ∂u 2x where j = 1, 2, . . . , N. 3x . Formula for Euler operator in 2D: (j) Mx (0,0) Lu(j) (x,y) = (j) My X X kx (−Dx ) (−Dy ) kx =0 ky =0 ∂ ky (j) ∂ukx x ky y ∂ ∂ ∂ = (j) − Dx (j) − Dy (j) ∂u ∂ux ∂uy + D2x ∂ 2 ∂ 3 ∂ +Dx Dy (j) +Dy (j) −Dx (j) (j) ∂u2x ∂uxy ∂u2y ∂u3x where j = 1, 2, . . . , N. ∂ ··· . Application: Testing Exactness Example: f = 3ux v 2 sin u −u3x sin u −6vvx cos u +2ux u2x cos u +8vx v2x where u(x) and v(x) • f is exact • After integration by parts (by hand): Z F = f dx = 4 vx2 + u2x cos u − 3 v 2 cos u . • Exactness test with Euler operator: f = 3ux v 2 sin u −u3x sin u −6vvx cos u +2ux u2x cos u +8vx v2x (0) Lu(x) f ∂f ∂f 2 ∂f − Dx + Dx ≡0 = ∂u ∂ux ∂u2x (0) Lv(x) f ∂f ∂f 2 ∂f = − Dx + Dx ≡0 ∂v ∂vx ∂v2x . Inverting Dx and Div Problem Statement in 1D • Example: f = 3ux v 2 sin u −u3x sin u −6vvx cos u +2ux u2x cos u +8vx v2x Z • Find F = • Result (by hand): f dx. So, f = Dx F F = 4 vx2 + u2x cos u − 3 v 2 cos u Mathematica cannot compute this integral! • Problem Statement in 2D Example: f = ux vy − u2x vy − uy vx + uxy vx where u(x, y) and v(x, y) • Find F = Div−1 f so, f = Div F • Result (by hand): F̃ = (uvy − ux vy , −uvx + ux vx ) • Problem Statement in 2D Example: f = ux vy − u2x vy − uy vx + uxy vx where u(x, y) and v(x, y) • Find F = Div−1 f so, f = Div F • Result (by hand): F̃ = (uvy − ux vy , −uvx + ux vx ) Mathematica cannot do this! Can this be done without integration by parts? Can this be reduced to single integral in one variable? • Problem Statement in 2D Example: f = ux vy − u2x vy − uy vx + uxy vx where u(x, y) and v(x, y) • Find F = Div−1 f so, f = Div F • Result (by hand): F̃ = (uvy − ux vy , −uvx + ux vx ) Mathematica cannot do this! Can this be done without integration by parts? Can this be reduced to single integral in one variable? Yes! With the Homotopy operator . Using the Homotopy Operator • Theorem (integration with homotopy operator): • In 1D: If f is exact then F = D−1 x f = Z f dx = Hu(x) f • In 2D: If f is a divergence then F = Div −1 f = (x) (y) (Hu(x,y) f, Hu(x,y) f ) • Homotopy Operator in 1D (variable x): Z Hu(x) f = 0 N 1X dλ (Iu(j) f )[λu] λ j=1 with integrand (j) Mx Iu(j) f = X k−1 X k=1 (j) uix k−(i+1) (−Dx ) i=0 ∂f (j) ∂ukx N is the number of dependent variables and (Iu(j) f )[λu] means that in Iu(j) f one replaces u → λu, ux → λux , etc. More general: u → λ(u − u0 ) + u0 ux → λ(ux − ux 0 ) + ux 0 etc. . Application of Homotopy Operator in 1D Example: f = 3ux v 2 sin u −u3x sin u −6vvx cos u +2ux u2x cos u +8vx v2x • Compute Iu f ∂f ∂f = u + (ux I − uDx ) ∂ux ∂u2x = 3uv 2 sin u − uu2x sin u + 2u2x cos u • Similarly, Iv f • Finally, ∂f ∂f = v + (vx I − vDx ) ∂vx ∂v2x = −6v 2 cos u + 8vx2 Z F = Hu(x) f = 0 = Z 1 1 dλ (Iu f + Iv f ) [λu] λ 3λ2 uv 2 sin(λu) − λ2 uu2x sin(λu) 0 +2λu2x cos(λu) − 6λv 2 cos(λu) + 8λvx2 dλ = 4vx2 + u2x cos u − 3v 2 cos u • Homotopy Operator in 2D (variables x and y): (x) Hu(x,y) f (y) Hu(x,y) f Z = N 1X 0 j=1 Z = (x) (Iu(j) f )[λu] N 1X 0 j=1 (y) (Iu(j) f )[λu] dλ λ dλ λ where (j) Mx (x) Iu(j) f = (j) My X X ky kX x −1 X kx =1 ky =0 (−Dx ) ix +iy uix x iy y ix ix =0 iy =0 kx −ix −1 −Dy ky −iy kx +ky −ix −iy −1 kx −ix −1 kx +ky kx ∂f (j) ∂ukx x ky y . Application of Homotopy Operator in 2D • Example: f = ux vy − u2x vy − uy vx + uxy vx • By hand: F̃ = (uvy − ux vy , −uvx + ux vx ) • Compute Iu(x) f ∂f ∂f + (ux I − uDx ) = u ∂ux ∂u2x 1 1 ∂f + uy I − uDy 2 2 ∂uxy 1 1 = uvy + uy vx − ux vy + uvxy 2 2 . • Similarly, Iv(x) f • ∂f =v = −uy v + uxy v ∂vx Hence, Z 1 dλ (x) (x) (x) F1 = Hu(x,y) f = Iu f + Iv f [λu] λ 0 Z 1 1 1 = λ uvy + uy vx − ux vy + uvxy − uy v + uxy v dλ 2 2 0 1 1 1 1 1 1 = uvy + uy vx − ux vy + uvxy − uy v + uxy v 2 4 2 4 2 2 . • Analogously, Z 1 dλ (y) (y) (y) F2 = Hu(x,y) f = Iu f + Iv f [λu] λ 0 ! Z 1 1 1 = λ −uvx − uv2x + ux vx + λ (ux v − u2x v) dλ 2 2 0 1 1 1 1 1 = − uvx − uv2x + ux vx + ux v − u2x v 2 4 4 2 2 • So, F= 1 uvy 2 + 41 uy vx − 12 ux vy + 14 uvxy − 12 uy v + 21 uxy v − 12 uvx − 14 uv2x + 41 ux vx + 21 ux v − 12 u2x v . Let K = F̃−F then 1 1 1 1 1 1 uv − u v − u v − uv + u v − uxy v y y x x y xy y 2 4 2 4 2 2 K= − 12 uvx + 14 uv2x + 43 ux vx − 21 ux v + 21 u2x v then Div K = 0 • Also, K = (Dy θ, −Dx θ) with θ = 12 uv − 14 uvx − 12 ux v (curl in 2D) Needed: Fast algorithm to remove curl terms (and strategy to avoid curl terms) . Computation of Conservation Laws for SWW Quick Recapitulation • Conservation law in (2+1) dimensions Dt ρ + ∇ · J = Dt ρ + Dx J1 + Dy J2 = 0 (on PDE) conserved density ρ and flux J = (J1 , J2 ) • Example: Shallow water wave (SWW) equations 1 ut + uux + vuy − 2 Ωv + hθx + θhx = 0 2 1 vt + uvx + vvy + 2 Ωu + hθy + θhy = 0 2 θt + uθx + vθy = 0 ht + hux + uhx + hvy + vhy = 0 • Typical density-flux pair: ρ(5) = vx θ − uy θ + 2Ωθ 1 4Ωuθ − 2uuy θ + 2uvx θ − hθθy (5) J = 2 4Ωvθ + 2vvx θ − 2vuy θ + hθθx Algorithm for PDEs in (2+1)-dimensions • Step 1: Construct the form of the density The SWW equations are invariant under the scaling symmetries (x, y, t, u, v, θ, h, Ω) → (λ−1 x, λ−1 y, λ−2 t, λu, λv, λθ, λh, λ2 Ω) and (x, y, t, u, v, θ, h, Ω) → (λ−1 x, λ−1 y, λ−2 t, λu, λv, λ2 θ, λ0 h, λ2 Ω) Construct a candidate density, for example, ρ = c1 Ωθ + c2 uy θ + c3 vy θ + c4 ux θ + c5 vx θ which is scaling invariant under both symmetries. . • Step 2: Determine the constants ci Compute E = −Dt ρ and remove time derivatives ∂ρ ∂ρ ∂ρ ∂ρ ∂ρ E = −( utx + uty + vtx + vty + θt ) ∂ux ∂uy ∂vx ∂vy ∂θ = c4 θ(uux + vuy − 2Ωv + 12 hθx + θhx )x + c2 θ(uux + vuy − 2Ωv + 12 hθx + θhx )y + c5 θ(uvx + vvy + 2Ωu + 12 hθy + θhy )x + c3 θ(uvx + vvy + 2Ωu + 21 hθy + θhy )y + (c1 Ω + c2 uy + c3 vy + c4 ux + c5 vx )(uθx + vθy ) Require that (0,0) (0,0) (0,0) (0,0) Lu(x,y) E = Lv(x,y) E = Lθ(x,y) E = Lh(x,y) E ≡ 0. . • Solution: c1 = 2, c2 = −1, c3 = c4 = 0, c5 = 1 gives ρ = 2Ωθ − uy θ + vx θ • Step 3: Compute the flux J E = θ(ux vx + uv2x + vx vy + vvxy + 2Ωux + 21 θx hy − ux uy − uuxy − uy vy − u2y v +2Ωvy − 21 θy hx ) +2Ωuθx + 2Ωvθy − uuy θx −uy vθy + uvx θx + vvx θy Apply the 2D homotopy operator: J = (J1 , J2 ) = Div −1 E= (x) (y) (Hu(x,y) E, Hu(x,y) E) . Compute Iu(x) E ∂E =u + ∂ux 1 1 ∂E uy I − uDy 2 2 ∂uxy 1 2 = uvx θ + 2Ωuθ + u θy − uuy θ 2 Similarly, compute 1 2 = vvy θ + v θy + uvx θ 2 1 2 (x) Iθ E = θ hy + 2Ωuθ − uuy θ + uvx θ 2 1 (x) Ih E = − θθy h 2 Iv(x) E . Next, J1 = = (x) Hu(x,y) E Z 1 Iu(x) E 0 Z = 0 1 dλ (x) (x) (x) + Iv E + Iθ E + Ih E [λu] λ 1 2 2 4λΩuθ + λ 3uvx θ + u θy − 2uuy θ + vvy θ 2 ! 1 2 1 2 1 + v θy + θ hy − θθy h dλ 2 2 2 2 1 1 2 = 2Ωuθ− uuy θ+ uvx θ+ vvy θ+ u θy 3 3 6 1 2 1 1 + v θy − hθθy + hy θ2 6 6 6 . Analogously, J2 = (y) Hu(x,y) E 2 1 1 2 1 2 = 2Ωvθ + vvx θ − vuy θ − uux θ − u θx − v θx 3 3 6 6 1 1 + hθθx − hx θ2 6 6 Hence, 112Ωuθ−4uuy θ+6uvx θ+2vvy θ+u2 θy +v 2 θy −hθθy +hy θ2 J= 6 12Ωvθ+4vvx θ−6vuy θ−2uux θ−u2 θx −v 2 θx +hθθx −hx θ2 . After removing the curl term 1 4Ωuθ − 2uuy θ + 2uvx θ − hθθy (5) J̃ = 2 4Ωvθ + 2vvx θ − 2vuy θ + hθθx Needed: Fast algorithm to remove curl terms (and strategy to avoid curl terms) Additional Examples • Example: Kadomtsev-Petviashvili (KP) Equation (ut + αuux + uxxx )x + σ 2 uyy = 0 parameter α ∈ IR and σ 2 = ±1. Equation be written as a conservation law Dt (ux ) + Dx (αuux + uxxx ) + Dy (σ 2 uy ) = 0. Exchange y and t and set ut = v ut = v vt 1 = − 2 (uxy + αu2x + αuuxx + uxxxx ) σ • Examples of conservation laws for KP equation (explicitly dependent on t, x, and y) Dt xux +Dx 3u2 −uxx −6xuux +xuxxx +Dy αxuy = 0 Dt yux +Dx y(αuux + uxxx ) +Dy σ 2 (yuy − u) = 0 √ √ 2y2 2y2 √ σ σ Dt tu + Dx α2 tu2 + tuxx + √ ut + √ uxxx 4 t 4 t √ √ √ ασ 2 y 2 + √ uux − x tut − αx tuux − x tuxxx 4 t √ y 2 uy yu +Dy x tuy + √ − √ = 0 4 t 2 t • More general conservation laws for KP equation: Dt f u + Dx f ( α2 u2 + uxx ) 2 +( σ2 f 0 y 2 − f x)(ut + αuux + u3x ) +Dy ( 21 f 0 y 2 − σ 2 f x)uy − f 0 yu = 0 Dt f yu + Dx f y( α2 u2 + uxx ) +y( σ2 +Dy 6 f 0 y 2 − f x)(ut + αuux + u3x ) y( 61 f 0 y 2 − σ 2 f x)uy +(σ 2 f x − 12 f 0 y 2 )u = 0 where f (t) is arbitrary function. . • Example: Potential KP Equation Replace u by ux and integrate with respect to x. uxt + αux u2x + u4x + σ 2 u2y = 0 • Examples of conservation laws (not explicitly dependent on x, y, t) 1 2 Dt (ux ) + Dx αux + u3x + Dy (σ 2 uy ) = 0 2 2 3 2 Dt (ux ) + Dx αux − u22x + 2ux u3x − σ 2 u2y 3 +Dy 2σ 2 ux uy = 0 Dt ux uy + Dx αu2x uy + ut uy + 2u3x uy − 2u2x uxy 1 3 2 2 +Dy σ uy − ux − ut ux + u22x = 0 3 Dt 2αuux u2x + 3uu4x − 3σ 2 u2y + Dx 2αut u2x + 3u2t −2αuux utx − 3utx u2x + 3ut u3x + 3ux ut 2x − 3uut 3x ) +Dy 6σ 2 ut uy = 0 Various generalizations exist . • Example: Khoklov-Zabolotskaya Equation (describes e.g. sound waves in nonlinear media) (ut − uux )x − u2y = 0 • Examples of conservation laws (with f (t)): Dt (ux ) + Dx (−uux ) + Dy (−uy ) = 0 1 2 1 0 2 Dt (f u) + Dx −(f x + 2 f y )(ut − uux ) − f u 2 +Dy (f x + 21 f 0 y 2 )uy − f 0 yu = 0 1 0 3 1 Dt (f yu) + Dx −(f xy + f y )(ut − uux ) − f yu2 6 2 1 0 2 1 0 3 +Dy (f xy + f y )uy − (f x + f y )u = 0 6 2 . • Example: Zakharov-Kuznetsov Equation (describes e.g. ion acoustic solitons in magnetic plasma) ut + αuux + β∇2 ux = 0 in 2-D, • ∇2 = ∂2 ∂x2 + ∂2 ∂y 2 Examples of conservation laws: α 2 Dt (u) + Dx u + βu2x + Dy βuxy = 0 2 2α 3 2 u − β(u2x − u2y ) + 2βu(u2x + u2y ) Dt u + D x 3 +Dy −2βux uy = 0 . 3β 2 3α 4 3 2 Dt u − (ux + uy ) + Dx u + 3βu2 u2x α 4 2 3β −6βu(u2x +u2y )+ (u22x −u22y ) α ! 6β 2 (ux (u3x +ux2y )+uy (u2xy +u3y )) − α ! 2 6β +Dy 3βu2 uxy + uxy (u2x + u2y ) = 0 α 2α 3 2 2 Dt tu − xu + Dx t( u − β(u2x − u2y ) α 3 2 α 2 2β +2βu(u2x + u2y )) − x( u + βu2x ) + ux α 2 α 1 −Dy 2β(tux uy + xuxy ) = 0 α . • Example: Navier’s Equation (describes e.g. wave motion in elastic solids) ∂2u ρ 2 = (λ + µ)∇(∇ · u) + µ∆u ∂t where u = (u, v, w), λ and µ are Lamé’s constants In components, ρu2t = (λ + µ) u2x + vxy + wxz + µ u2x + u2y + u2z ρv2t = (λ + µ) uxy + v2y + wyz + µ v2x + v2y + v2z ρw2t = (λ + µ) uxz + vyz + w2z + µ w2x + w2y + w2z . • Examples of densities (fluxes are long): ρ(1) = ρut ρ(2) = ρvt ρ(3) = ρwt ρ(4) = ux (vtz − wty ) − vx (utz − wtx ) + wx (uty − vtx ) ρ(5) = uy (vtz − wty ) + vx wty − vy utz − wx vty + wy uty ρ(6) = (uy − vx )wtz − (uz − wx )vtz + (vz − wy )utz ρ(7) = ρ(vt utz −wt (uty −vtx ))+µ uy wzz +vx (uxz −wyy −wzz ) + vy uyz + vz uzz + wx (vxx − uxy ) − wy uyy and many more.... . Conclusions and Future Work • The power of Euler and homotopy operators: I Testing exactness I −1 Integration by parts, D−1 , and Div x • Integration of non-exact expressions Example: f = ux v + uvx + u2 u2x R R 2 f dx = uv + u u2x dx • Treat broader class of PDEs (other than those of evolution type) • Full implementation in Mathematica . Thank You Software packages in Mathematica Codes are available via the Internet: URL: http://inside.mines.edu/∼whereman/ Publications 1. W. Hereman, P. J. Adams, H. L. Eklund, M. S. Hickman, and B. M. Herbst, Direct Methods and Symbolic Software for Conservation Laws of Nonlinear Equations, In: Advances of Nonlinear Waves and Symbolic Computation, Ed.: Z. Yan, Nova Science Publishers, New York (2009), Chapter 2, pp. 19-79. 2. W. Hereman, M. Colagrosso, R. Sayers, A. Ringler, B. Deconinck, M. Nivala, and M. S. Hickman, Continuous and Discrete Homotopy Operators and the Computation of Conservation Laws. In: Differential Equations with Symbolic Computation, Eds.: D. Wang and Z. Zheng, Birkhäuser Verlag, Basel (2005), Chapter 15, pp. 249-285. 3. W. Hereman, Symbolic computation of conservation laws of nonlinear partial differential equations in multi-dimensions, Int. J. Quan. Chem. 106(1), 278-299 (2006). 4. W. Hereman, B. Deconinck, and L. D. Poole, Continuous and discrete homotopy operators: A theoretical approach made concrete, Math. Comput. Simul. 74(4-5), 352-360 (2007).