In a rocket, hydrogen is burned with air, both reactants supplied as gases at Po, To. The

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In a rocket, hydrogen is burned with air, both reactants supplied as gases at Po, To. The combustion is adiabatic and the mixture is stoichiometric (100% theoretical air). Find the products dew point and the adiabatic flame temperature (~2500 K).
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Fundamentals of Thermodynamics

ISBN: 978-0471152323

6th edition

Authors: Richard E. Sonntag, Claus Borgnakke, Gordon J. Van Wylen

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