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Modelling of turbulent reacting flows with gaseous fuels in a combustion chamber

✍ Scribed by Celalettin Çelik; Ahimet Arisoy; Osman F. Genceli

Book ID
107756893
Publisher
Elsevier Science
Year
1996
Tongue
English
Weight
633 KB
Volume
75
Category
Article
ISSN
0016-2361

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An experimental method was used to determine the intensity of turbulence and the Lagrangian correlation coefficient in a GH2-GOX rocket combustion chamber. The method consisted of injecting a tracer gas at an upstream point on the centerline of the combustion chamber while taking gas samples along a