Author:
Matesanz A,Velazquez A,Rodriguez M,Ryantsansev Y,Kourdiumov V
Publisher
American Institute of Aeronautics and Astronautics
Reference14 articles.
1. +Mo(w12+0,3) Wo P up dY02 = M02(2-7-ll-12)-wo 2
2. Eqs. 13;Onedifferentialtotal
3. 1 1 1 0.000 1
4. [I]Frenklach M. "Reductionof Chemical Reduction Models". Numerical Approaches to Combustion Modelling. Progress in Aeronautics and Astronautics,vol. 135,1991.
5. Reduced Kinetic Mechanisms for Applications in Combustion Systems