Source code for pysph.sph.wc.basic

"""
Basic WCSPH Equations
#####################
"""

from pysph.sph.equation import Equation


[docs]class TaitEOS(Equation): r"""**Tait equation of state for water-like fluids** :math:`p_a = \frac{c_{0}^2\rho_0}{\gamma}\left( \left(\frac{\rho_a}{\rho_0}\right)^{\gamma} -1\right)` References ---------- .. [Cole1948] H. R. Cole, "Underwater Explosions", Princeton University Press, 1948. .. [Batchelor2002] G. Batchelor, "An Introduction to Fluid Dynamics", Cambridge University Press, 2002. .. [Monaghan2005] J. Monaghan, "Smoothed particle hydrodynamics", Reports on Progress in Physics, 68 (2005), pp. 1703-1759. """ def __init__(self, dest, sources, rho0, c0, gamma, p0=0.0): r""" Parameters ---------- rho0 : float reference density of fluid particles c0 : float maximum speed of sound expected in the system gamma : float constant p0 : float reference pressure in the system (defaults to zero). Notes ----- The reference speed of sound, c0, is to be taken approximately as 10 times the maximum expected velocity in the system. The particle sound speed is given by the usual expression: :math:`c_a = \sqrt{\frac{\partial p}{\partial \rho}}` """ self.rho0 = rho0 self.rho01 = 1.0/rho0 self.c0 = c0 self.gamma = gamma self.gamma1 = 0.5*(gamma - 1.0) self.B = rho0*c0*c0/gamma self.p0 = p0 super(TaitEOS, self).__init__(dest, sources)
[docs] def loop(self, d_idx, d_rho, d_p, d_cs): ratio = d_rho[d_idx] * self.rho01 tmp = pow(ratio, self.gamma) d_p[d_idx] = self.p0 + self.B * (tmp - 1.0) d_cs[d_idx] = self.c0 * pow(ratio, self.gamma1)
[docs]class TaitEOSHGCorrection(Equation): r"""**Tait Equation of State with Hughes and Graham Correction** .. math:: p_a = \frac{c_{0}^2\rho_0}{\gamma}\left( \left(\frac{\rho_a}{\rho_0}\right)^{\gamma} -1\right) where .. math:: \rho_{a}=\begin{cases}\rho_{a} & \rho_{a}\geq\rho_{0}\\ \rho_{0} & \rho_{a}<\rho_{0}\end{cases}` References ---------- .. [Hughes2010] J. P. Hughes and D. I. Graham, "Comparison of incompressible and weakly-compressible SPH models for free-surface water flows", Journal of Hydraulic Research, 48 (2010), pp. 105-117. """ def __init__(self, dest, sources, rho0, c0, gamma): r""" Parameters ---------- rho0 : float reference density c0 : float reference speed of sound gamma : float constant Notes ----- The correction is to be applied on boundary particles and imposes a minimum value of the density (rho0) which is set upon instantiation. This correction avoids particle sticking behaviour at walls. """ self.rho0 = rho0 self.rho01 = 1.0/rho0 self.c0 = c0 self.gamma = gamma self.gamma1 = 0.5*(gamma - 1.0) self.B = rho0*c0*c0/gamma super(TaitEOSHGCorrection, self).__init__(dest, sources)
[docs] def loop(self, d_idx, d_rho, d_p, d_cs): if d_rho[d_idx] < self.rho0: d_rho[d_idx] = self.rho0 ratio = d_rho[d_idx] * self.rho01 tmp = pow(ratio, self.gamma) d_p[d_idx] = self.B * (tmp - 1.0) d_cs[d_idx] = self.c0 * pow(ratio, self.gamma1)
[docs]class MomentumEquation(Equation): r"""**Classic Monaghan Style Momentum Equation with Artificial Viscosity** .. math:: \frac{d\mathbf{v}_{a}}{dt}=-\sum_{b}m_{b}\left(\frac{p_{b}} {\rho_{b}^{2}}+\frac{p_{a}}{\rho_{a}^{2}}+\Pi_{ab}\right) \nabla_{a}W_{ab} where .. math:: \Pi_{ab}=\begin{cases} \frac{-\alpha\bar{c}_{ab}\mu_{ab}+\beta\mu_{ab}^{2}}{\bar{\rho}_{ab}} & \mathbf{v}_{ab}\cdot\mathbf{r}_{ab}<0;\\ 0 & \mathbf{v}_{ab}\cdot\mathbf{r}_{ab}\geq0; \end{cases} with .. math:: \mu_{ab}=\frac{h\mathbf{v}_{ab}\cdot\mathbf{r}_{ab}} {\mathbf{r}_{ab}^{2}+\eta^{2}}\\ \bar{c}_{ab} = \frac{c_a + c_b}{2}\\ \bar{\rho}_{ab} = \frac{\rho_a + \rho_b}{2} References ---------- .. [Monaghan1992] J. Monaghan, Smoothed Particle Hydrodynamics, "Annual Review of Astronomy and Astrophysics", 30 (1992), pp. 543-574. """ def __init__(self, dest, sources, c0, alpha=1.0, beta=1.0, gx=0.0, gy=0.0, gz=0.0, tensile_correction=False): r""" Parameters ---------- c0 : float reference speed of sound alpha : float produces a shear and bulk viscosity beta : float used to handle high Mach number shocks gx : float body force per unit mass along the x-axis gy : float body force per unit mass along the y-axis gz : float body force per unit mass along the z-axis tensilte_correction : bool switch for tensile instability correction (Default: False) """ self.alpha = alpha self.beta = beta self.gx = gx self.gy = gy self.gz = gz self.c0 = c0 self.tensile_correction = tensile_correction super(MomentumEquation, self).__init__(dest, sources)
[docs] def initialize(self, d_idx, d_au, d_av, d_aw, d_dt_cfl): d_au[d_idx] = 0.0 d_av[d_idx] = 0.0 d_aw[d_idx] = 0.0 d_dt_cfl[d_idx] = 0.0
[docs] def loop(self, d_idx, s_idx, d_rho, d_cs, d_p, d_au, d_av, d_aw, s_m, s_rho, s_cs, s_p, VIJ, XIJ, HIJ, R2IJ, RHOIJ1, EPS, DWIJ, WIJ, WDP, d_dt_cfl): rhoi21 = 1.0/(d_rho[d_idx]*d_rho[d_idx]) rhoj21 = 1.0/(s_rho[s_idx]*s_rho[s_idx]) vijdotxij = VIJ[0]*XIJ[0] + VIJ[1]*XIJ[1] + VIJ[2]*XIJ[2] piij = 0.0 if vijdotxij < 0: cij = 0.5 * (d_cs[d_idx] + s_cs[s_idx]) muij = (HIJ * vijdotxij)/(R2IJ + EPS) piij = -self.alpha*cij*muij + self.beta*muij*muij piij = piij*RHOIJ1 # compute the CFL time step factor _dt_cfl = 0.0 if R2IJ > 1e-12: _dt_cfl = abs(HIJ * vijdotxij/R2IJ) + self.c0 d_dt_cfl[d_idx] = max(_dt_cfl, d_dt_cfl[d_idx]) tmpi = d_p[d_idx]*rhoi21 tmpj = s_p[s_idx]*rhoj21 fij = WIJ/WDP Ri = 0.0 Rj = 0.0 # tensile instability correction if self.tensile_correction: fij = fij*fij fij = fij*fij if d_p[d_idx] > 0: Ri = 0.01 * tmpi else: Ri = 0.2*abs(tmpi) if s_p[s_idx] > 0: Rj = 0.01 * tmpj else: Rj = 0.2 * abs(tmpj) # gradient and correction terms tmp = (tmpi + tmpj) + (Ri + Rj)*fij d_au[d_idx] += -s_m[s_idx] * (tmp + piij) * DWIJ[0] d_av[d_idx] += -s_m[s_idx] * (tmp + piij) * DWIJ[1] d_aw[d_idx] += -s_m[s_idx] * (tmp + piij) * DWIJ[2]
[docs] def post_loop(self, d_idx, d_au, d_av, d_aw, d_dt_force): d_au[d_idx] += self.gx d_av[d_idx] += self.gy d_aw[d_idx] += self.gz acc2 = (d_au[d_idx]*d_au[d_idx] + d_av[d_idx]*d_av[d_idx] + d_aw[d_idx]*d_aw[d_idx]) # store the square of the max acceleration d_dt_force[d_idx] = acc2
[docs]class MomentumEquationDeltaSPH(Equation): r"""**Momentum equation defined in JOSEPHINE and the delta-SPH model** .. math:: \frac{du_{i}}{dt}=-\frac{1}{\rho_{i}}\sum_{j}\left(p_{j}+p_{i}\right) \nabla_{i}W_{ij}V_{j}+\mathbf{g}_{i}+\alpha hc_{0}\rho_{0}\sum_{j} \pi_{ij}\nabla_{i}W_{ij}V_{j} where .. math:: \pi_{ij}=\frac{\mathbf{u}_{ij}\cdot\mathbf{r}_{ij}} {|\mathbf{r}_{ij}|^{2}} References ---------- .. [Marrone2011] S. Marrone et al., "delta-SPH model for simulating violent impact flows", Computer Methods in Applied Mechanics and Engineering, 200 (2011), pp 1526--1542. .. [Cherfils2012] J. M. Cherfils et al., "JOSEPHINE: A parallel SPH code for free-surface flows", Computer Physics Communications, 183 (2012), pp 1468--1480. """ def __init__(self, dest, sources, rho0, c0, alpha=1.0): r""" Parameters ---------- rho0 : float reference density c0 : float reference speed of sound alpha : float coefficient used to control the intensity of the diffusion of velocity Notes ----- Artificial viscosity is used in this momentum equation and is controlled by the parameter :math:`\alpha`. This form of the artificial viscosity is similar but not identical to the Monaghan-style artificial viscosity. """ self.alpha = alpha self.c0 = c0 self.rho0 = rho0 super(MomentumEquationDeltaSPH, self).__init__(dest, sources)
[docs] def loop(self, d_idx, s_idx, d_rho, d_cs, d_p, d_au, d_av, d_aw, s_m, s_rho, s_cs, s_p, VIJ, XIJ, HIJ, R2IJ, RHOIJ1, EPS, WIJ, DWIJ): # src paricle volume mj/rhoj Vj = s_m[s_idx]/s_rho[s_idx] # viscous contribution second part of eqn (5b) in [Maronne2011] vijdotxij = VIJ[0]*XIJ[0] + VIJ[1]*XIJ[1] + VIJ[2]*XIJ[2] fac = self.alpha * HIJ * self.c0 * self.rho0 piij = vijdotxij/(R2IJ + EPS) # gradient and viscous terms eqn 5b in [Maronne2011] tmp = fac * piij * Vj/d_rho[d_idx] # accelerations d_au[d_idx] += tmp * DWIJ[0] d_av[d_idx] += tmp * DWIJ[1] d_aw[d_idx] += tmp * DWIJ[2]
[docs]class ContinuityEquationDeltaSPHPreStep(Equation): r"""**Continuity equation with dissipative terms** See :class:`pysph.sph.wc.basic.ContinuityEquationDeltaSPH` The matrix :math:`L_a` is multiplied to :math:`\nabla W_{ij}` in the :class:`pysph.sph.scheme.WCSPHScheme` class by using :class:`pysph.sph.wc.kernel_correction.GradientCorrectionPreStep` and :class:`pysph.sph.wc.kernel_correction.GradientCorrection`. """
[docs] def initialize(self, d_idx, d_gradrho): d_gradrho[d_idx*3 + 0] = 0.0 d_gradrho[d_idx*3 + 1] = 0.0 d_gradrho[d_idx*3 + 2] = 0.0
[docs] def loop(self, d_idx, d_arho, s_idx, d_rho, s_rho, s_m, d_gradrho, DWIJ): rhoi = d_rho[d_idx] rhoj = s_rho[s_idx] Vj = s_m[s_idx]/rhoj # renormalized density of eqn (5a) d_gradrho[d_idx*3 + 0] += (rhoj - rhoi) * DWIJ[0] * Vj d_gradrho[d_idx*3 + 1] += (rhoj - rhoi) * DWIJ[1] * Vj d_gradrho[d_idx*3 + 2] += (rhoj - rhoi) * DWIJ[2] * Vj
[docs]class ContinuityEquationDeltaSPH(Equation): r"""**Continuity equation with dissipative terms** :math:`\frac{d\rho_a}{dt} = \sum_b \rho_a \frac{m_b}{\rho_b} \left( \boldsymbol{v}_{ab}\cdot \nabla_a W_{ab} + \delta \eta_{ab} \cdot \nabla_{a} W_{ab} (h_{ab}\frac{c_{ab}}{\rho_a}(\rho_b - \rho_a)) \right)` References ---------- .. [Marrone2011] S. Marrone et al., "delta-SPH model for simulating violent impact flows", Computer Methods in Applied Mechanics and Engineering, 200 (2011), pp 1526--1542. """ def __init__(self, dest, sources, c0, delta=0.1): r""" Parameters ---------- c0 : float reference speed of sound delta : float coefficient used to control the intensity of diffusion of density """ self.c0 = c0 self.delta = delta super(ContinuityEquationDeltaSPH, self).__init__(dest, sources)
[docs] def loop(self, d_idx, d_arho, s_idx, s_m, d_rho, s_rho, DWIJ, XIJ, R2IJ, HIJ, EPS, d_gradrho, s_gradrho): rhoi = d_rho[d_idx] rhoj = s_rho[s_idx] Vj = s_m[s_idx]/rhoj fac = -2.0 * (rhoj - rhoi)/(R2IJ + EPS) psix = fac*XIJ[0] - d_gradrho[d_idx*3 + 0] - s_gradrho[s_idx*3 + 0] psiy = fac*XIJ[1] - d_gradrho[d_idx*3 + 1] - s_gradrho[s_idx*3 + 1] psiz = fac*XIJ[2] - d_gradrho[d_idx*3 + 2] - s_gradrho[s_idx*3 + 2] psidotdwij = psix*DWIJ[0] + psiy*DWIJ[1] + psiz*DWIJ[2] # standard term with dissipative penalization eqn (5a) d_arho[d_idx] += self.delta * HIJ * self.c0 * psidotdwij * Vj
[docs]class UpdateSmoothingLengthFerrari(Equation): r"""**Update the particle smoothing lengths** :math:`h_a = hdx \left(\frac{m_a}{\rho_a}\right)^{\frac{1}{d}}` References ---------- .. [Ferrari2009] A. Ferrari et al., "A new 3D parallel SPH scheme for free surface flows", Computers and Fluids, 38 (2009), pp. 1203--1217. """ def __init__(self, dest, sources, dim, hdx): r""" Parameters ---------- dim : float number of dimensions hdx : float scaling factor Notes ----- Ideally, the kernel scaling factor should be determined from the kernel used based on a linear stability analysis. The default value of (hdx=1) reduces to the formulation suggested by Ferrari et al. who used a Cubic Spline kernel. Typically, a change in the smoothing length should mean the neighbors are re-computed which in PySPH means the NNPS must be updated. This equation should therefore be placed as the last equation so that after the final corrector stage, the smoothing lengths are updated and the new NNPS data structure is computed. Note however that since this is to be used with incompressible flow equations, the density variations are small and hence the smoothing lengths should also not vary too much. """ self.dim1 = 1./dim self.hdx = hdx super(UpdateSmoothingLengthFerrari, self).__init__(dest, sources)
[docs] def loop(self, d_idx, d_rho, d_h, d_m): # naive estimate of particle volume Vj = d_m[d_idx]/d_rho[d_idx] d_h[d_idx] = self.hdx * pow(Vj, self.dim1)
[docs]class PressureGradientUsingNumberDensity(Equation): r"""Pressure gradient discretized using number density: .. math:: \frac{d \boldsymbol{v}_a}{dt} = -\frac{1}{m_a}\sum_b (\frac{p_a}{V_a^2} + \frac{p_b}{V_b^2})\nabla_a W_{ab} """
[docs] def initialize(self, d_idx, d_au, d_av, d_aw): d_au[d_idx] = 0.0 d_av[d_idx] = 0.0 d_aw[d_idx] = 0.0
[docs] def loop(self, d_idx, s_idx, d_m, d_rho, s_rho, d_au, d_av, d_aw, d_p, s_p, d_V, s_V, DWIJ): # particle volumes Vi = 1./d_V[d_idx] Vj = 1./s_V[s_idx] Vi2 = Vi * Vi Vj2 = Vj * Vj # pressure gradient term p_i = d_p[d_idx] pj = s_p[s_idx] pij = p_i*Vi2 + pj*Vj2 # accelerations tmp = -pij * 1.0/(d_m[d_idx]) d_au[d_idx] += tmp * DWIJ[0] d_av[d_idx] += tmp * DWIJ[1] d_aw[d_idx] += tmp * DWIJ[2]