Convective-film cooling of vortex rotor blades in GTE high-temperature turbines

被引：0
|
作者：
Gorelov, YG
Kopylov, IS
Kazurov, VF
机构：
来源：
IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA | 2001年 / 02期
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中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
We present the results of the comparison experimental study of cooling efficiency for vortex rotor blades in high-pressure turbines with different variants of film curtain for the blade profile under conditions of speed-up of TFE thermodynamic cycle to T-2 = 1700 K.
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页码：34 / 38
页数：5
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