INFLUENCE OF DIFFUSER INLET VELOCITY PROFILE ON FLOW PATTERN.

被引：0
|
作者：
Turilov, A.M.
Shalaev, G.M.
机构：
来源：
Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika) | 1985年 / 28卷 / 03期
关键词：
AIRCRAFT ENGINES; JET AND TURBINE - Diffusers;
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学科分类号：
摘要：
In gas turbine combustion chamber diffusers the velocity profile at the entrance is often nonuniform. We present the results of an experimental study of the flow structures in a diffuser for various forms of inlet velocity profile nonuniformity. We show the variation of the average and maximal characteristics of the flow along the diffuser channel.
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页码：78 / 81
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