DEVELOPMENT OF NEW SINGLE AND HIGH-DENSITY HEAT-FLUX GAUGES FOR UNSTEADY HEAT TRANSFER MEASUREMENTS FOR A ROTATING TRANSONIC TURBINE

被引:0
|
作者
Celestina, Richard [1 ]
Sperling, Spencer [1 ]
Christensen, Louis [1 ]
Mathison, Randall [1 ]
Aksoy, Hakan [2 ]
Liu, Jong [2 ]
机构
[1] Ohio State Univ, Columbus, OH 43210 USA
[2] Honeywell Aerosp, Phoenix, AZ USA
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 7C | 2020年
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents the development and implementation of a new generation of double-sided heat- flux gauges at The Ohio State University Gas Turbine Laboratory (GTL) along with heat transfer measurements for film-cooled airfoils in a single-stage high-pressure transonic turbine operating at design corrected conditions. Double-sided heat flux gauges are a critical part of turbine cooling studies, and the new generation improves upon the durability and stability of previous designs while also introducing high-density layouts that provide better spatial resolution. These new customizable high-density double-sided heat flux gauges allow for multiple heat transfer measurements in a small geometric area such as immediately downstream of a row of cooling holes on an airfoil. Two high-density designs are utilized: Type A consists of 9 gauges laid out within a 5 mm by 2.6 mm (0.20 inch by 0.10 inch) area on the pressure surface of an airfoil, and Type B consists of 7 gauges located at points of predicted interest on the suction surface. Both individual and high-density heat flux gauges are installed on the blades of a transonic turbine experiment for the second build of the High- Pressure Turbine Innovative Cooling program (HPTIC2). Run in a short duration facility, the singlestage high-pressure turbine operated at design-corrected conditions (matching corrected speed, flow function, and pressure ratio) with forward and aft purge flow and film- cooled blades. Gauges are placed at repeated locations across different cooling schemes in a rainbow rotor configuration. Airfoil filmcooling schemes include round, fan, and advanced shaped cooling holes in addition to uncooled airfoils. Both the pressure and suction surfaces of the airfoils are instrumented at multiple wetted distance locations and percent spans from roughly 10% to 90%. Results from these tests are presented as both timeaverage values and time-accurate ensemble averages in order to capture unsteady motion and heat transfer distribution created by strong secondary flows and cooling flows.
引用
收藏
页数:14
相关论文
共 50 条
  • [1] Unsteady Heat Transfer and Pressure Measurements on the Airfoils of a Rotating Transonic Turbine With Multiple Cooling Configurations
    Nickol, Jeremy B.
    Mathison, Randall M.
    Dunn, Michael G.
    Liu, Jong S.
    Malak, Malak F.
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2017, 139 (09):
  • [2] UNSTEADY HEAT TRANSFER AND PRESSURE MEASUREMENTS ON THE AIRFOILS OF A ROTATING TRANSONIC TURBINE WITH MULTIPLE COOLING CONFIGURATIONS
    Nickol, Jeremy B.
    Mathison, Randall M.
    Dunn, Michael G.
    Liu, Jong S.
    Malak, Malak F.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5A, 2016,
  • [3] CRITICAL HEAT-FLUX AND HEAT-TRANSFER FOR HIGH HEAT-FLUX APPLICATIONS
    BOYD, RD
    POWELL, LN
    SCHLUTER, LL
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1986, 29 (02) : 337 - 340
  • [4] Unsteady rotor heat transfer in a transonic turbine stage
    Didier, F
    Dénos, R
    Arts, T
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2002, 124 (04): : 614 - 622
  • [5] MICROSENSORS FOR HIGH HEAT-FLUX MEASUREMENTS
    HAGER, JM
    LANGLEY, LW
    ONISHI, S
    DILLER, TE
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 1993, 7 (03) : 531 - 534
  • [6] Aerodynamic and heat-flux measurements with predictions on a modern one and one-half state high pressure transonic turbine
    Haldeman, CW
    Dunn, MG
    Barter, JW
    Green, BR
    Bergholz, RF
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2005, 127 (03): : 522 - 531
  • [7] Endwall heat transfer measurements in a transonic turbine cascade
    Giel, PW
    Thurman, DR
    Van Fossen, GJ
    Hippensteele, SA
    Boyle, RJ
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1998, 120 (02): : 305 - 313
  • [8] PHASE-RESOLVED HEAT-FLUX MEASUREMENTS ON THE BLADE OF A FULL-SCALE ROTATING TURBINE
    DUNN, MG
    SEYMOUR, PJ
    WOODWARD, SH
    GEORGE, WK
    CHUPP, RE
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1989, 111 (01): : 8 - 19
  • [9] Simultaneous heat flux and velocity measurements in a transonic turbine cascade
    Holmberg, DG
    Diller, TE
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2005, 127 (03): : 502 - 506
  • [10] Validation of heat-flux predictions on the outer air seal of a transonic turbine blade
    Clark, JP
    Polanka, MD
    Meininger, M
    Praisner, TJ
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2006, 128 (03): : 589 - 595