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Volumn 3, Issue , 2000, Pages

Rotor / stator heat transfer measurements and CFD predictions for short-duration turbine rig tests

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; BOUNDARY LAYERS; COMPUTATION THEORY; COMPUTATIONAL FLUID DYNAMICS; FORECASTING; GAGES; HEAT FLUX; HEAT TRANSFER COEFFICIENTS; REYNOLDS NUMBER; SYSTEMATIC ERRORS; TEST FACILITIES; TESTING; TURBINE COMPONENTS; TURBINES; TURBOMACHINE BLADES; UNCERTAINTY ANALYSIS;

EID: 84955152521     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0208     Document Type: Conference Paper
Times cited : (15)

References (11)
  • 3
    • 0006650308 scopus 로고    scopus 로고
    • Heat-flux measurements for the rotor of a full-stage turbine: Part 1-time-averaged results
    • Dunn, M. G., "Heat-Flux Measurements for the Rotor of a Full-Stage Turbine: Part 1-Time-Averaged Results," J. of Turbomachinery, Vol. 108, pp. 90-97.
    • J. of Turbomachinery , vol.108 , pp. 90-97
    • Dunn, M.G.1
  • 4
    • 5244272137 scopus 로고
    • Investigation of unsteady flow through a transonic turbine stage: Part II-data/prediction comparison for time-averaged and phase-resolved pressure data
    • July 16-18, Orlando, FL
    • Dunn, M.G., Bennett, W., Delaney, R., and Rao, K., 1990, "Investigation of Unsteady Flow Through a Transonic Turbine Stage: Part II-Data/Prediction Comparison for Time-Averaged and Phase-Resolved Pressure Data," AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference, Paper No. 90-2409, July 16-18, Orlando, FL.
    • (1990) AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference, Paper No. 90-2409
    • Dunn, M.G.1    Bennett, W.2    Delaney, R.3    Rao, K.4
  • 5
    • 0031455972 scopus 로고    scopus 로고
    • Investigation of the heat-island effect for heat-flux measurements in short-duration facilities
    • Dunn, M. G, Kim, J., and Rae, W. J., 1997, "Investigation of the Heat-Island Effect for Heat-Flux Measurements in Short-Duration Facilities", J. Turbomachinery, Vol. 119, pp. 753-760.
    • (1997) J. Turbomachinery , vol.119 , pp. 753-760
    • Dunn, M.G.1    Kim, J.2    Rae, W.J.3
  • 7
  • 10
    • 0344354613 scopus 로고
    • The tailored-interface hypersonic shock tunnel
    • Wittliff, C.E., Wilson, M.R., and Hertzberg, A., 1959, "The Tailored-Interface Hypersonic Shock Tunnel," J. Aerospace Sciences, Vol. 26, No.4, pp. 219-228.
    • (1959) J. Aerospace Sciences , vol.26 , Issue.4 , pp. 219-228
    • Wittliff, C.E.1    Wilson, M.R.2    Hertzberg, A.3
  • 11
    • 0006650306 scopus 로고    scopus 로고
    • Influence of non-isothermal button gage surface temperature in heat flux measurement applications
    • Ziles, David A. and Abhari, Reza S., "Influence of Non-Isothermal Button Gage Surface Temperature in Heat Flux Measurement Applications", IMECE, 1999.
    • (1999) IMECE
    • Ziles David, A.1    Abhari Reza, S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.