moved to AeroUtils/
------------------------------------------------------------------------------- Reynold's number ------------------------------------------------------------------------------- Form: ReynoldsNumber rE = ReynoldsNumber( rho, v, mu, x ) ------------------------------------------------------------------------------- ------ Inputs ------ rho (1,:) Density v (1,:) Velocity mu (1,:) Dynamic viscosity x (1,:) Characteristic length ------- Outputs ------- rE (1,:) Reynold's number ------------------------------------------------------------------------------- References: http://en.wikipedia.org/wiki/Reynolds_number -------------------------------------------------------------------------------
Common: General/StdAtm Common: Graphics/Plot2D Thermal: ThermalAnalysis/SutherlandsLaw Thermal: ThermalAnalysis/TemperatureStagnation