INVESTIGATION OF THE TIP CLEARANCE FLOW INSIDE AND AT THE EXIT OF A COMPRESSOR ROTOR PASSAGE .1. MEAN VELOCITY-FIELD

被引：18

作者：

PANDYA, A ^{[1
]}

LAKSHMINARAYANA, B ^{[1
]}

机构：

[1] PENN STATE UNIV, DEPT AEROSP ENGN, UNIVERSITY PK, PA 16802 USA

来源：

JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME | 1983年 / 105卷 / 01期

关键词：

D O I：

10.1115/1.3227389

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

引用

页码：1 / 12

页数：12

共 48 条

[1] INVESTIGATION OF THE TIP CLEARANCE FLOW INSIDE AND AT THE EXIT OF A COMPRESSOR ROTOR PASSAGE .2. TURBULENCE PROPERTIES
PANDYA, A
LAKSHMINARAYANA, B
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1983, 105 (01): : 13 - 17
[2] Investigation on the tip clearance flow field in a transonic compressor rotor
Gui, Xingmin
Wang, Tongqing
Yu, Qing
Li, Yunmin
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 19 (05): : 553 - 558
[3] 3-DIMENSIONAL FLOW FIELD IN THE TIP REGION OF A COMPRESSOR ROTOR PASSAGE .1. MEAN VELOCITY PROFILES AND ANNULUS WALL BOUNDARY-LAYER
LAKSHMINARAYANA, B
POUAGARE, M
DAVINO, R
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1982, 104 (04): : 760 - 771
[4] THE EFFECTS OF TIP CLEARANCE ON FLOW FIELD AND LOSSES IN A COMPRESSOR ROTOR
LAKSHMINARAYANA, B
ZHANG, J
MURTHY, KNS
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1990, 14 (04): : 273 - 281
[5] TIP CLEARANCE FLOW IN A COMPRESSOR ROTOR PASSAGE AT DESIGN AND OFF-DESIGN CONDITIONS
LAKSHMINARAYANA, B
PANDYA, A
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1984, 106 (03): : 570 - 577
[6] Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
Suder, KL
Celestina, ML
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1996, 118 (02): : 218 - 229
[7] Three-dimensional flow field inside a compressor rotor tip region
Hangkong Dongli Xuebao/Journal of Aerospace Power, 1997, 12 (02): : 167 - 171
[8] Three-dimensional mean flow field at both inlet and exit of an isolated axial compressor rotor passage in different conditions
Ma, Hongwei
Jiang, Haokang
Dong, Yuxi
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2000, 15 (02): : 119 - 123
[9] EFFECTS OF TIP CLEARANCE AND OPERATING CONDITIONS ON THE FLOW STRUCTURE AND TURBULENCE WITHIN AN AXIAL COMPRESSOR ROTOR PASSAGE
Li, Yuanchao
Chen, Huang
Tan, David
Katz, Joseph
PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2A, 2016,
[10] Development of three-dimensional turbulent flow field at exit of an axial compressor rotor passage
Ma, Hongwei
Jiang, Haokang
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2000, 15 (02): : 113 - 118

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