Is automated combustion preprocessing and propulsion simulation powerful software for researchers and professional engineers. It can be helpful for students that specialize in combustion and thermodynamic processes as well. The programs can greatly boost your efficiency by eliminating wasted time spent in looking up formulas, and then performing the same calculations over and over by hand. This software solves a wide range of common engineering problems related to gas turbine and jet engines quickly and efficiently. The program can help for those, who want to deal with design and development of laboratory combustion facility.
The LOXCOM 2.6 software predicts the steady-state properties of a gas turbine combustion chamber or other combustion devices such as for example Bunsen burner. An annular combustor of gas turbine engine is included by default in the software for modeling combustion and heat transfer through a wall. In addition a can combustor can easily be analyzed as well. The software allows modeling of flameless combustion as well by means of temperature, mole, and mass fraction distribution (et cetera) according to proposed mathematical model. Such model uses a term of recirculation ratio proposed by (Levy et al.). A variable content of air can be used as well. For steady state problems all relevant information will be given as text or graphical representation. User defined fuel option is also available. The application can be related to MATLAB program in order to graphically represent the results which were calculated by the software. The program can be applied to analyses of stoichiometric or lean combustion of pure or blended fuels.

For more information about the software, please, visit the LOXCOM 2.6 on our partners website.