Path: Propulsion/Gas
% Computes the combustion temperature of a gas mixture. Since version 2. -------------------------------------------------------------------------- Form: t = CombTemp( nR, nP, hR, hP, cPP ) -------------------------------------------------------------------------- ------ Inputs ------ nR (n) Number of moles of each reactant nP (m) Number of moles of each product hR (n) Heat of formation of each reactant hP (m) Heat of formation of each product cPP (m) Heat capacity of each product ------- Outputs ------- t Combustion temperature --------------------------------------------------------------------------
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