Path: Propulsion/Gas
% Computes the ratio of specific heats of a gas mixture. -------------------------------------------------------------------------- Form: [gammaM, nM] = Gamma( cP, n ) -------------------------------------------------------------------------- ------ Inputs ------ cP (:) Specific heats of the constituents (cal/mole deg K) n (:) Number of moles of each constituent ------- Outputs ------- gammaM (:) Ratio of specific heat of the mixture (cal/mole deg K) nM (:) Number of moles in the mixture -------------------------------------------------------------------------- References: Martinez-Sanchez, M. "16.53 Course Notes" M.I.T. 1979. --------------------------------------------------------------------------
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