moved to AeroUtils/
-------------------------------------------------------------------------- Sutherland's law for dynamic viscosity. Defaults are for air. Defaults are mks. Type SutherlandsLaw for a demo. -------------------------------------------------------------------------- Form: SutherlandsLaw mu = SutherlandsLaw( t, mu0, t0, s ) mu = SutherlandsLaw( t) -------------------------------------------------------------------------- ------ Inputs ------ t (1,:) Temperature mu0 (1,1) Reference viscosity t0 (1,1) Reference temperature s (1,1) Sutherland temperature ------- Outputs ------- mu (1,:) Dynamic viscosity -------------------------------------------------------------------------- References: http://www.cfd-online.com/Wiki/Sutherland_law --------------------------------------------------------------------------
Common: Graphics/Plot2D