Adiabatic Flame Temperature Calculation: A Simple Approach for General CHONS Fuels
Author:
Affiliation:
1. Lilley & Associates
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-817
Reference18 articles.
1. correctionis2000 K. The procedure is: 1. GuessT ofproducts 2. Calculate Q = P- R 3. IfQ is positive, take newT =T -∆T IfQisnegative, take newT =T +∆T
2. temperatures by about 2000 K, from 5000+ to 3000+
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