A Split-Operator, Finite-Difference Solution for Axisymmetric Laminar-Jet Biffusion Flames
Author:
Affiliation:
1. Sandia Laboratories, Livermore, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60873
Reference12 articles.
1. 5Pohl, J. H. "Kinetics of Nitric Oxide and Carbon Monoxide in Combustion Systems," M.S. Thesis, Massachusetts Inst.of Technology, 1972.
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