Application of the ball-spine algorithm to design axial-flow compressor blade

被引：0

作者：

机构：

[1] Madadi, A.

[2] Kermani, M.J.

[3] Nili-Ahmadabadi, M.

来源：

| 1600年 / Sharif University of Technology卷 / 21期

关键词：

Axial flow - Axial-flow compressors - Geometry;

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引用

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[31] MEAN VELOCITY AND DECAY CHARACTERISTICS OF THE GUIDEVANE AND STATOR BLADE WAKE OF AN AXIAL-FLOW COMPRESSOR
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[32] Method of Scientific Profiling of the Subsonic Axial-Flow Compressor's Stage Blade.
Stangiu, V.
1987, 49 : 57 - 62
[33] MEAN VELOCITY AND DECAY CHARACTERISTICS OF THE GUIDEVANE AND STATOR BLADE WAKE OF AN AXIAL-FLOW COMPRESSOR
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[34] Application of Surrogate Models for Through-Flow Calculation in an Axial-Flow Compressor
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[35] EFFECT OF INTERACTION BETWEEN WAKES FROM BLADE ROWS IN AN AXIAL-FLOW COMPRESSOR ON NOISE GENERATED BY BLADE INTERACTION
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[36] EFFECT OF INTERACTION BETWEEN WAKES FROM BLADE ROWS IN AN AXIAL-FLOW COMPRESSOR ON NOISE GENERATED BY BLADE INTERACTION
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[37] AXIAL-FLOW COMPRESSOR DESIGN OPTIMIZATION .2. THROUGHFLOW ANALYSIS
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SATTA, A
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[38] DESIGN OF AXIAL-FLOW COMPRESSOR BLADES WITH INCLINED STREAM SURFACE AND VARYING AXIAL VELOCITY
INOUE, M
IKUI, T
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BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1979, 22 (171): : 1190 - 1197
[39] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATION
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[40] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATION
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