the question is about: Investigate the potential for the use of ammonia as a gas turbine fuel. Aspects to consider include the heat
of combustion and the adiabatic flame temperature. Given your knowledge of heat of formation and heat of
reaction, can you demonstrate how the adiabatic flame temperature is determined?
How do these compare with other typical fuels, e.g. methane, kerosene, hydrogen? What other
environmental problems might be associated with the use of ammonia as a fuel?
one last thing i want to mention. can you do a extra small paragraph that summarize the long paragraphs, because this question is part of the group project, so i need this one summarized to read it orally during the presentation. the presentation will be from 3 min to 5 long.
thank you.
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