コード例 #1
0
ファイル: taylor_bar.py プロジェクト: yang7857854/pysph
    def create_equations(self):
        equations = [

            # Properties computed set from the current state
            Group(
                equations=[
                    # p
                    MieGruneisenEOS(dest='bar',
                                    sources=None,
                                    gamma=gamma,
                                    r0=r0,
                                    c0=C,
                                    S=S),

                    # vi,j : requires properties v00, v01, v10, v11
                    VelocityGradient2D(dest='bar', sources=[
                        'bar',
                    ]),

                    # rij : requires properties s00, s01, s11
                    VonMisesPlasticity2D(flow_stress=Yo,
                                         dest='bar',
                                         sources=None),
                ], ),

            # Acceleration variables are now computed
            Group(equations=[

                # arho
                ContinuityEquation(dest='bar', sources=['bar']),

                # au, av
                MomentumEquationWithStress(dest='bar', sources=['bar']),

                # au, av
                MonaghanArtificialViscosity(dest='bar',
                                            sources=['bar'],
                                            alpha=0.5,
                                            beta=0.5),

                # au av
                MonaghanBoundaryForce(dest='bar', sources=['plate'],
                                      deltap=dx),

                # ae
                EnergyEquationWithStress(dest='bar',
                                         sources=['bar'],
                                         alpha=0.5,
                                         beta=0.5,
                                         eta=0.01),

                # a_s00, a_s01, a_s11
                HookesDeviatoricStressRate(dest='bar', sources=None),

                # ax, ay, az
                XSPHCorrection(dest='bar', sources=[
                    'bar',
                ], eps=0.5),
            ])  # End Acceleration Group
        ]  # End Group list
        return equations
コード例 #2
0
    def create_equations(self):
        equations = [

            # update smoothing length
            # Group(
            #     equations = [
            #         UpdateSmoothingLengthFromVolume(dest='plate',      sources=['plate', 'projectile'], dim=dim, k=hdx),
            #         UpdateSmoothingLengthFromVolume(dest='projectile', sources=['plate', 'projectile'], dim=dim, k=hdx),
            #     ],
            #     update_nnps=True,
            # ),

            # compute properties from the current state
            Group(equations=[
                # EOS (compute the pressure using  one of the EOSs)

                # MieGruneisenEOS(dest='plate',      sources=None, gamma=gamma1, r0=ro1 , c0=C1, S=S1),
                # MieGruneisenEOS(dest='projectile', sources=None, gamma=gamma2, r0=ro2 , c0=C2, S=S2),
                StiffenedGasEOS(
                    dest='plate', sources=None, gamma=gamma1, r0=ro1, c0=C1),
                StiffenedGasEOS(dest='projectile',
                                sources=None,
                                gamma=gamma2,
                                r0=ro2,
                                c0=C2),

                # compute the velocity gradient tensor
                VelocityGradient3D(dest='plate', sources=['plate']),
                VelocityGradient3D(dest='projectile', sources=['projectile']),

                # # stress
                VonMisesPlasticity2D(
                    dest='plate', sources=None, flow_stress=Yo1),
                VonMisesPlasticity2D(
                    dest='projectile', sources=None, flow_stress=Yo2),

                # # artificial stress to avoid clumping
                MonaghanArtificialStress(dest='plate', sources=None, eps=0.3),
                MonaghanArtificialStress(
                    dest='projectile', sources=None, eps=0.3),
            ]),

            # accelerations (rho, u, v, ...)
            Group(equations=[

                # continuity equation
                ContinuityEquation(dest='plate',
                                   sources=['projectile', 'plate']),
                ContinuityEquation(dest='projectile',
                                   sources=['projectile', 'plate']),

                # momentum equation
                MomentumEquationWithStress(dest='projectile',
                                           sources=[
                                               'projectile',
                                               'plate',
                                           ]),
                MomentumEquationWithStress(dest='plate',
                                           sources=[
                                               'projectile',
                                               'plate',
                                           ]),

                # energy equation:
                EnergyEquationWithStress(dest='plate',
                                         sources=[
                                             'projectile',
                                             'plate',
                                         ],
                                         alpha=avisc_alpha,
                                         beta=avisc_beta,
                                         eta=avisc_eta),
                EnergyEquationWithStress(dest='projectile',
                                         sources=[
                                             'projectile',
                                             'plate',
                                         ],
                                         alpha=avisc_alpha,
                                         beta=avisc_beta,
                                         eta=avisc_eta),

                # avisc
                MonaghanArtificialViscosity(dest='plate',
                                            sources=['projectile', 'plate'],
                                            alpha=avisc_alpha,
                                            beta=avisc_beta),
                MonaghanArtificialViscosity(dest='projectile',
                                            sources=['projectile', 'plate'],
                                            alpha=avisc_alpha,
                                            beta=avisc_beta),

                # updates to the stress term
                HookesDeviatoricStressRate(
                    dest='plate', sources=None, shear_mod=1.),
                HookesDeviatoricStressRate(
                    dest='projectile', sources=None, shear_mod=1.),

                # position stepping
                XSPHCorrection(dest='plate', sources=['plate'], eps=xsph_eps),
                XSPHCorrection(
                    dest='projectile', sources=['projectile'], eps=xsph_eps),
            ]),
        ]  # End Group list

        return equations