Question: In a rocket, hydrogen is burned with air, both reactants supplied as gases at Po, To. The combustion is adiabatic and the mixture is stoichiometeric

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

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The reaction equation is H 2 O2 O 2 376 N 2 H 2 O 376 v O2 N 2 The balance of hydrogen is done now ... View full answer

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