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 stoichiometric

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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The reaction equation is H V02 O 376 N HO 376 V02 N The balance of hydrogen is done now ... View full answer

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