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Volumn 15, Issue 9, 2004, Pages 1910-1916

Flow visualization on the linear compressor cascade endwall using oil flows and laser Doppler anemometry

Author keywords

Flow angle; Laser Doppler anemometry; Linear compressor cascade; Oil flow visualization; Wall shear stress

Indexed keywords

FLOW VISUALIZATION; FRICTION; LASER DOPPLER VELOCIMETERS; SHEAR STRESS; WIND TUNNELS;

EID: 7444230981     PISSN: 09570233     EISSN: None     Source Type: Journal    
DOI: 10.1088/0957-0233/15/9/031     Document Type: Article
Times cited : (22)

References (16)
  • 1
    • 0002762562 scopus 로고
    • Full three-dimensional measurements of the cross-flow separation region of a 6:1 prolate spheroid
    • Chesnakas C J and Simpson R L 1994 Full three-dimensional measurements of the cross-flow separation region of a 6:1 prolate spheroid Exp. Fluids 17 68-74
    • (1994) Exp. Fluids , vol.17 , pp. 68-74
    • Chesnakas, C.J.1    Simpson, R.L.2
  • 4
    • 0028526712 scopus 로고
    • Tip leakage flow in a linear compressor cascade
    • Kang S and Hirsch C 1994 Tip leakage flow in a linear compressor cascade ASME J. Turbomach. 116 657-64
    • (1994) ASME J. Turbomach. , vol.116 , pp. 657-664
    • Kang, S.1    Hirsch, C.2
  • 8
    • 0029310877 scopus 로고
    • A five-velocity-component laser-Doppler velocimeter for measurements of a three-dimensional turbulent boundary layer
    • Ölçmen S M and Simpson R L 1995 A five-velocity-component laser-Doppler velocimeter for measurements of a three-dimensional turbulent boundary layer Meas. Sci. Technol. 6 702-16
    • (1995) Meas. Sci. Technol. , vol.6 , pp. 702-716
    • Ölçmen, S.M.1    Simpson, R.L.2
  • 11
    • 0942278270 scopus 로고
    • The motion of a thin oil sheet under the steady boundary layer on a body
    • Squires L C 1962 The motion of a thin oil sheet under the steady boundary layer on a body J. Fluid Mech. 11 161-79
    • (1962) J. Fluid Mech. , vol.11 , pp. 161-179
    • Squires, L.C.1
  • 12
    • 0026143134 scopus 로고
    • Tip leakage flow in axial compressors
    • Storer J A and Cumpsty N A 1991 Tip leakage flow in axial compressors ASME J. Turbomach. 113 252-9
    • (1991) ASME J. Turbomach. , vol.113 , pp. 252-259
    • Storer, J.A.1    Cumpsty, N.A.2
  • 14
    • 85034750816 scopus 로고    scopus 로고
    • Measurement of the tip-gap turbulence structure for a stationary end-wall in a low-speed compressor cascade
    • at press
    • Tang G, Simpson R L and Tian Q 2004 Measurement of the tip-gap turbulence structure for a stationary end-wall in a low-speed compressor cascade AIAA J. at press
    • (2004) AIAA J.
    • Tang, G.1    Simpson, R.L.2    Tian, Q.3
  • 16
    • 0342819167 scopus 로고    scopus 로고
    • Measurement of three-dimensional crossflow separation
    • Wetzel T G, Simpson R L and Chesnakas C J 1998 Measurement of three-dimensional crossflow separation AIAA J. 36 557-64
    • (1998) AIAA J. , vol.36 , pp. 557-564
    • Wetzel, T.G.1    Simpson, R.L.2    Chesnakas, C.J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.