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Searched refs:U_infty (Results 1 – 2 of 2) sorted by relevance

/honee/qfunctions/
H A Dblasius.h73 CeedScalar U_infty = Norm3(S_infty.Y.velocity); in BlasiusSolution() local
74 CeedScalar eta = x[1] * sqrt(U_infty / (nu * (x0 + x[0] - x_inflow))); in BlasiusSolution()
82 *t12 = mu * U_infty * f[2] * sqrt(U_infty / (nu * (x0 + x[0] - x_inflow))); in BlasiusSolution()
85 Y[1] = U_infty * f[1]; in BlasiusSolution()
86 Y[2] = 0.5 * sqrt(nu * U_infty / (x0 + x[0] - x_inflow)) * (eta * f[1] - f[0]); in BlasiusSolution()
108 const CeedScalar U_infty = Norm3(S_infty.Y.velocity); in ICsBlasius() local
110 const CeedScalar x0 = U_infty * S_infty.U.density / (mu * 25 / Square(delta0)); in ICsBlasius()
135 const CeedScalar U_infty = Norm3(S_infty.Y.velocity); in Blasius_Inflow() local
136 …const CeedScalar x0 = U_infty * rho_0 / (gas.mu * 25 / Square(context->delta0)… in Blasius_Inflow()
190 const CeedScalar U_infty = Norm3(S_infty.Y.velocity); in Blasius_Inflow_Jacobian() local
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/honee/problems/
H A Dblasius.c23 CeedScalar U_infty = Norm3(S_infty.Y.velocity); in CompressibleBlasiusResidual() local
27 …PetscScalar Ma = Mach(gas, S_infty.Y.temperature, U_infty), Pr = Prandtl(gas), gamma = HeatCapacit… in CompressibleBlasiusResidual()