DescriptionCalculates the theoretical thermodynamic properties for an equilibrium mixture. The program can be applied to equipment such as compressors, turbines, nozzles, engines, shock tubes, heat exchangers, and chemical processing equipment.
Month - $30
Week - $20
Day - $15
Initiation Fee - $200
The program can handle any of the following, specific problems:
(a) Calculate chemical equilibrium composition for thermodynamic states
(b) Calculate theoretical rocket performance for finite or infinite area combustion chamber
(c) Calculate Champman-Jouguet detonations
(d) Calculate shock tube parameters for both incident and reflected shocks
To calculate the equilibrium composition of a composition, the user is
required to supply the state of the equilibrium mixture. The user provides
the program with any two thermodynamic-state functions from the following
Solving the rocket problem requires the input of data type (3) and type (1) or (2).
The thermodynamic data calculated by the program include conductivity, viscosity, specific heats, sound speed, equilibrium temperature and pressure, enthalpy, entropy, internal energy, and many others.