catalyticChamberFoam

Solver for catalytic chambers of monopropellant thrusters with Two chemical reactions, one for a surface gas (heterogeneous reaction ) and another for interstitial gas ( homogeneous reaction ), mass Transfers for porous media with mass diffusion coefficient calculation of Chagmant - Esnokg Theory. Mass and Heat transport relations are based on Wakao. For the doctoral theses: "ROBLEDO ASENCIO, J. C. Estudo numérico do processo de decomposição em câmaras catalíticas de propulsores monopropelentes. 2020. 189 p. IBI: <8JMKD3MGP3W34R/3UGHFGH>. (sid.inpe.br/mtc-m21c/2019/12.04.15.16-TDI). Tese (Doutorado em Combustão e Propulsão) - Instituto Nacional de Pesquisas Espaciais (INPE), São José dos Campos, 2019. Disponível em: ibi:8JMKD3MGP3W34R/3UGHFGH." (http://urlib.net/rep/8JMKD3MGP3W34R/3UGHFGH) and previously work: Asencio, J. R., Savonov, R. I., & Marques, R. I.. (2020). An Open-source Solver to Model the Catalytic Decomposition of Monopropellants for Space Thrusters. Journal of Aerospace Technology and Management, 12(J. Aerosp. Technol. Manag., 2020 12), e1120. https://doi.org/10.5028/jatm.v12.1111. Please if you use it, don't forget to reference it. Suggestions are welcome! File catalyticChamberFoamV1.0 contains the original code made in 2019 to the thesis and there is a test as well.