WorldofAerospace.googlepages.com Contact Us | Sitemap | Home Calculate Equation of State Parameters  Method to Calculate the Equation of State, Pressure, Density and Temperature Parameters Aerospace Equation of State The equation of the state is given as, P = row*R*T where, row is the density. To calculate the Pressure using the equation of state, Input Value of Density in kg/m^3 Input Value of Temperature in K. Input Specific Gas Constant value, R in J/kgK.  The default value of Gas constant is 287 J/kg.K   Performing the calculation gives the pressure in terms of N/m^2.   To calculate the Temperature using the equation of state, Input Value of Density in kg/m^3 Input Value of Pressure in N/m^2 Input Specific Gas Constant value, R in J/kg.k   Performing the calculation gives the temperature in terms of K. To calculate the density using the equation of state, Input Value of Temperature in Kelvin K Input Value of Pressure in N/m^2 Input Specific Gas Constant Value, R in J/kg.K Performing the calculation gives the density in terms of kg/m^3.   Download Free Program to Calculate the Equation of State Parameters 