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The temperature rise in combustion chamber (AT) depends on the fuel to air ratio S and air temperature upstream of the combustion chamber for
The temperature rise in combustion chamber (AT) depends on the fuel to air ratio S and air temperature upstream of the combustion chamber for an upstream temperature of 650 K, this relation may be expressed as: AT(K) = af +b=3,393x10"f+21.08 For n-octane fuel determine the following: a. Calculate the fuel to air ratio if the temperature rise in combustion chamber is 950 K b. Calculate the equivalence ratio . c. Write down the chemical reaction equation.
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Thermodynamics for Engineers
Authors: Kenneth A. Kroos, Merle C. Potter
1st edition
1133112862, 978-113311286
