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Combustion of Liquid and Gaseous Fuels in a Supersonic Combustor

✍ Scribed by J. L. Le; H. C. Bai; A. A. Mishunin; A. V. Starov


Book ID
110442052
Publisher
SP MAIK Nauka/Interperiodica
Year
2003
Tongue
English
Weight
238 KB
Volume
39
Category
Article
ISSN
0010-5082

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Spray characteristics like mean drop diameter and spray cone angle play an important role in the process of combustion within a gas turbine combustor. In order to study their effects on wall and exit temperature distributions and combustion efficiency in the combustor, a numerical model of a typical