| /honee/qfunctions/ |
| H A D | riemann_solver.h | 101 RoeWeights r = RoeSetup(left.U.density, right.U.density); in ComputeHLLSpeeds_Roe()
122 RoeWeights r = RoeSetup(left.U.density, right.U.density); in ComputeHLLSpeeds_Roe_fwd()
123 RoeWeights dr = RoeSetup_fwd(left.U.density, right.U.density, dleft.U.density, dright.U.density); in ComputeHLLSpeeds_Roe_fwd()
217 CeedScalar fact = side.U.density * (s_side - u_side) / (s_side - s_star); in RiemannFlux_HLLC_Star()
218 CeedScalar denom = side.U.density * (s_side - u_side); in RiemannFlux_HLLC_Star()
227 side.U.E_total / side.U.density // in RiemannFlux_HLLC_Star()
237 CeedScalar fact = side.U.density * (s_side - u_side) / (s_side - s_star); in RiemannFlux_HLLC_Star_fwd()
238 …CeedScalar dfact = (side.U.density * (ds_side - du_side) + dside.U.density * (s_side - u_side)) / … in RiemannFlux_HLLC_Star_fwd()
240 CeedScalar denom = side.U.density * (s_side - u_side); in RiemannFlux_HLLC_Star_fwd()
241 CeedScalar ddenom = side.U.density * (ds_side - du_side) + dside.U.density * (s_side - u_side); in RiemannFlux_HLLC_Star_fwd()
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| H A D | newtonian_state.h | 14 CeedScalar density; member
25 U[0] = s.density; in UnpackState_U()
55 return e_internal + e_kinetic + s.Y.pressure / s.U.density; in TotalSpecificEnthalpy()
61 …de_internal + de_kinetic + ds.Y.pressure / s.U.density - s.Y.pressure / Square(s.U.density) * ds.U… in TotalSpecificEnthalpy_fwd()
66 for (CeedInt i = 0; i < 3; i++) Y.velocity[i] = U.momentum[i] / U.density; in StatePrimitiveFromConservative()
68 CeedScalar e_total = U.E_total / U.density; in StatePrimitiveFromConservative()
71 Y.pressure = (HeatCapacityRatio(gas) - 1) * U.density * e_internal; in StatePrimitiveFromConservative()
78 dY.velocity[i] = (dU.momentum[i] - s.Y.velocity[i] * dU.density) / s.U.density; in StatePrimitiveFromConservative_fwd()
82 CeedScalar e_total = s.U.E_total / s.U.density; in StatePrimitiveFromConservative_fwd()
83 CeedScalar de_total = (dU.E_total - e_total * dU.density) / s.U.density; in StatePrimitiveFromConservative_fwd()
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| H A D | blasius.h | 110 const CeedScalar x0 = U_infty * S_infty.U.density / (mu * 25 / Square(delta0)); in ICsBlasius()
114 State s = BlasiusSolution(context, x, x0, x_inflow, S_infty.U.density, &t12); in ICsBlasius()
134 const CeedScalar rho_0 = S_infty.U.density; in Blasius_Inflow()
153 s.U.density = s_int.U.density; in Blasius_Inflow()
189 const CeedScalar rho_0 = S_infty.U.density; in Blasius_Inflow_Jacobian()
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| H A D | gaussianwave.h | 42 …const CeedScalar e_kinetic = 0.5 * S_infty.U.density * Dot3(S_infty.Y.velocity, S_infty.Y.velocity… in IC_GaussianWave()
46 U[0] = S_infty.U.density * perturbation; in IC_GaussianWave()
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| H A D | newtonian.h | 230 …const CeedScalar body_force[5] = {0, s.U.density * g[0], s.U.density * g[1], s.U.density * g[2], D… in RHSFunction_Newtonian()
295 …const CeedScalar body_force[5] = {0, s.U.density * g[0], s.U.density * g[1], s.U.density * g[2], D… in IFunction_Newtonian_Integrand()
406 …const CeedScalar dbody_force[5] = {0, ds.U.density * g[0], ds.U.density * g[1], ds.U.density * g[2… in IJacobian_Newtonian_Integrand()
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| H A D | monitor_totalkineticenergy.h | 25 v[0][i] = wdetJ * 0.5 * s.U.density * Dot3(s.Y.velocity, s.Y.velocity); in MonitorTotalKineticEnergy()
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| H A D | sgs_dd_training.h | 48 …ComputeSgsDDInputs(grad_velo_aniso, km_A_ij, delta, gas.mu / s.U.density, eigenvectors, inputs, &g… in ComputeSGS_DDAnisotropicTrainingDataNodal()
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| H A D | stabilization.h | 76 const CeedScalar rho = s.U.density; in Tau_diagPrim()
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| H A D | sgs_dd_model.h | 90 ComputeSgsDD_Fused(grad_velo_aniso, km_A_ij, delta, gas.mu / s.U.density, km_sgs, sgsdd_ctx); in ComputeSgsDDNodal_Fused()
134 …ComputeSgsDDInputs(grad_velo_aniso, km_A_ij, delta, gas.mu / s.U.density, eigenvectors, model_inpu… in ComputeSgsDDNodal_Sequential_Inputs()
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| /honee/qfunctions/spanstats/ |
| H A D | turbulence.h | 56 v[TURB_MEAN_DENSITY][i] = wdetJ * s.U.density; in ChildStatsCollection()
62 v[TURB_MEAN_DENSITY_TEMPERATURE][i] = wdetJ * s.U.density * s.Y.temperature; in ChildStatsCollection()
63 …v[TURB_MEAN_DENSITY_TEMPERATURE_FLUX_X][i] = wdetJ * s.U.density * s.Y.temperature * s.Y.velocity[… in ChildStatsCollection()
64 …v[TURB_MEAN_DENSITY_TEMPERATURE_FLUX_Y][i] = wdetJ * s.U.density * s.Y.temperature * s.Y.velocity[… in ChildStatsCollection()
65 …v[TURB_MEAN_DENSITY_TEMPERATURE_FLUX_Z][i] = wdetJ * s.U.density * s.Y.temperature * s.Y.velocity[… in ChildStatsCollection()
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| /honee/doc/ |
| H A D | examples.md | 85 where $\rho_\infty, u_\infty$ are the freestream (inflow) density and velocity respectively.
115 (example-density-current)=
144 - Axis of density current cylindrical anomaly, or `(0,0,0)` for spherically symmetric
300 At the inflow, the velocity is prescribed by the Blasius soution profile, density is set constant, …
301 Using `weakT: true`, density is allowed to float and temperature is set constant.
485 …s taken to be the acoustic speed while the reference density $\rho_{ref}$ is just the local densit…
497 …ortional to the element length in the direction of the density gradient unit vector. This density …
545 …ction-diffusion, which holds density $\rho$ and momentum density $\rho \bm u$ constant while advec…
560 …We have solved {eq}`eq-advection` applying zero energy density $E$, and no-flux for $\bm{u}$ on th…
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| H A D | theory.md | 20 …mass density, $U$ the momentum density (defined as $\bm{U}=\rho \bm{u}$, where $\bm{u}$ is the vec…
44 \leftarrow\textrm{ volume mass density}\\
45 \leftarrow\textrm{ momentum density}\\
46 \leftarrow\textrm{ energy density}
337 …he exact solution to the Euler equations, and the so called {ref}`example-density-current` problem.
560 … it weakly enforces velocity, with the option of weakly enforcing either density or temperature us…
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| H A D | references.bib | 64 …title = {Numerical solutions of a non-linear density current: A benchmark solution and compari…
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