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Experimental and numerical investigation of airfoil clocking and inter-blade-row gap effects on axial compressor performance

被引：0
|
作者：
Saren, VE
Savin, NM
Dorney, DJ
Sondak, DL
机构：
[1] Virginia Commonwealth Univ, Dept Mech Engn, Richmond, VA 23284 USA
[2] Cent Inst Aviat Motors, Moscow, Russia
[3] Boston Univ, Boston, MA 02215 USA
来源：
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES | 1998年 / 15卷 / 04期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
An experimental and computational research program has been performed to study the effects of stator indexing (clocking) in a high-speed axial compressor stage with an inlet guide vane. The work is directed at determining the basic now mechanisms causing the performance variations associated with airfoil clocking. A comparison of the results obtained for two axial gaps between the rotor and the stator has been carried out to determine the role of potential interaction between blade rows as the airfoils are clocked.
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页码：235 / 251
页数：17
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