![]() Absolute or Dynamic Viscosity Online ConverterĪir dynamic viscosity at varying temperature and constant pressures (1-10 000 bara, 14.5 - 145 000 psia):Īir kinematic viscosity at varying temperature and constant pressures (1-10 000 bara, 14.5 - 145 000 psia):Īir dynamic and kinematic viscosity at gas-liquid equilibrium pressure:ĭynamic (absolute) and kinematic viscosity of air at 1 atmosphere pressure, at temperatures given as ☏:įor full table with kinematic viscosity - rotate the screen! Temperatureĭynamic (absolute) and kinematic viscosity of air at 1 atmosphere pressure, at temperatures given as ☌:Ĭentipoise, gram/(centimeter second) = poise, kilogram/meter second =newton second/square meter = pascal second, pound/(foot hour) , pound/(foot second), reyn.See also other properties of Air at varying temperature and pressure: Density and specific weight at varying temperature, Density at varying pressure, Diffusion Coefficients for Gases in Air, Prandtl Number, Specific heat at varying temperature and Specific heat at varying pressure, Thermal Conductivity, Thermal Diffusivity, Properties at gas-liquid equilibrium conditions and Air thermophysical properties at standard conditions and Composition and molecular weight,Īs well as dynamic and kinematic viscosity of ammonia, benzene, butane, carbon dioxide, ethane, ethanol, ethylene, methane, methanol, nitrogen, oxygen, propane and water.Īir dynamic and kinematic viscosity at atmospheric pressure and varying temperature: Temperature Choose the actual unit of temperature: While the kinematic viscosity is given as cSt, m 2/s, and ft 2/s The output dynamic viscosity is given as Pa*s, N*s/m 2, cP, mPa*s, lb f*s/ft 2 and lb m/(ft*h), The calculator below can be used to calculate air dynamic or kinematic viscosity at given temperatures and atmospheric pressure. Tabulated values and viscosity units conversion are given below the figures. Absolute or dynamic viscosity is used to calculate Reynold's Number to determine if a fluid flow is laminar, transient or turbulent. The thermodynamic properties of air along the saturation curve are given in Table 1 these properties for the liquid and gaseous air-in Table 2.The viscosity of a fluid is a measure of its resistance to gradual deformation by shear stress or tensile stress.įor further definitions, go to Absolute (dynamic) and kinematic viscosity. The equilibrium dissociation degree can be calculated according to the Saha equation. This implies the transition of air into the plasma state. Their equilibrium concentration can be derived from the isotherm equations of the respective reactions.Īt temperatures higher than 2000 K and moderate pressures the nitrogen and oxygen start to dissociate, and at temperatures exceeding 4000 K and atmospheric pressure the ionization of oxygen, nitrogen, and other components becomes evident. The nitrogen reacts with oxygen producing various oxides: N 2O, NO, NO 2, NO 3. The normal condensation temperature of air is -191.4☌, the normal boiling temperature -194☌.Īt elevated temperatures air undergoes some physicochemical transformations. Liquid air at atmospheric pressure behaves practically as an ideal solution following the Raoult's Law. The normal (at 0.1013 MPa) boiling (condensation) temperature of the oxygen is equal- 183☌, that of the nitrogen -195.8☌. Where v denotes specific volume u is specific internal energy R is the gas constant for air.Īt low temperatures the air is liquified.
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