Ensemble-average three-dimensional velocity measurement in the tip region of axial rotor with tip clearance

Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

Volumn 22, Issue 2, 2004, Pages 196-200

  Zhu, Xiao Cheng ^a   Guo, Qiang ^a   Du, Zhao Hui ^a  

^a SHANGHAI JIAO TONG UNIVERSITY   (China)

Author keywords

Axial rotor; Leakage flow; PDA; Tip clearance

Indexed keywords

AXIAL ROTOR; LEAKAGE FLOW; LEAKAGE VORTEX; PARTICLE DOPPLER AEROMETER; TIP CLEARANCE;

DOPPLER EFFECT; ROTORS; THREE DIMENSIONAL; VELOCITY MEASUREMENT;

FLOW OF FLUIDS;

EID: 4344629872     PISSN: 02581825     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

1. WISLER D C. Loss reduction in axial-flow compressor through low-speed model testing [J]. Journal of Turbomachinery, 1985, 107: 354-363.
2. LAKSHMINARAYAN B et al. Three-dimensional flow field in the tip region of a compressor rotor passage-part1: mean velocity profiles and annulus wall boundary layer [J]. Journal of Engineering for Power, 1982, 104: 761-772.
3. LAKSHIMINARAYANA B, DA VINO R, POUAGARE M. Three-dimensional flow field in the tip region of a compressor rotor passage-part II: turbulence properties [J]. Journal of Engineering for Power, 1982, 104: 772-781.
4. WISLER D C, MOSSEY P W. Gas velocity measurements within a compressor rotor passage using the laser Doppler velocimeter [J]. Journal of Engineering for Power, 1973, 95(2): 91-97.
5. LAKSHIMINARYANA B, SITARAM N, ZHANG J. End-wall and profile losses in low-speed axial flow compressor rotor [J]. Journal of engineering for gas turbines and power, 1986, 108: 22-31.
6. LAKSHMINARAYANA B,ZACCARIA M, MARATHE B. The structure of tip clearance flow in axial flow compressors [J]. Journal of turbomachinery, 1995, 17: 336-347.
7. HUNTER I H, CUMPSTY N A. Casing wall boundary-layer development through an isolated compressor rotor [J]. Journal of Engineering for Power, 1982, 104: 805-818