The current upper-bound limitation for the calculation of thermodynamic and transport properties is 100 atm (10 MPa). For the simulation of higher total pressure rocket nozzles, coefficients for enthalpy, specific heat, compressibility, thermal conductivity, and viscosity are required.
The current upper-bound limitation for the calculation of thermodynamic and transport properties is 100 atm (10 MPa). For the simulation of higher total pressure rocket nozzles, coefficients for enthalpy, specific heat, compressibility, thermal conductivity, and viscosity are required.