Find the products dew point and the adiabatic flame


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Q: 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). You should solve the problem step by step.You must include all the units which are needed to solve the given problem.

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Mechanical Engineering: Find the products dew point and the adiabatic flame
Reference No:- TGS02011381

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