Time-resolved temperature and velocity field measurements in gas turbine film cooling flows with mainstream turbulence

被引:13
|
作者
Strausswald, Michael [1 ]
Abram, Christopher [2 ]
Sander, Tobias [1 ]
Beyrau, Frank [2 ]
Pfitzner, Michael [1 ]
机构
[1] Univ Bundeswehr Munchen, Inst Thermodynam, Werner Heisenberg Weg 39, D-85577 Neubiberg, Germany
[2] Otto von Guericke Univ, Inst Fluid Dynam & Thermodynam, Univ Pl 2, D-39106 Magdeburg, Germany
关键词
FREE-STREAM TURBULENCE; TRACER; PARTICLES; ZNO;
D O I
10.1007/s00348-020-03087-2
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Gas turbine film cooling strategies must provide adequate cooling performance under high levels of mainstream turbulence. Detailed information about the structure, dynamics and transport of the cooling films is needed to understand the flow physics and develop suitable numerical simulation tools. Here, we study film cooling flows in a wind tunnel with mainstream turbulence generated by an active turbulence grid. Gas temperature and velocity fields are measured using a laser-imaging method based on thermographic phosphor tracer particles. By replacing the previously used tracer BaMgAl10O17:Eu2+ with ZnO, significant gains in accuracy and precision could be achieved. The increased sensitivity (similar to 1%/K) of ZnO led to a threefold improvement in the single-shot, single-pixel temperature precision to +/- 5 K. The smaller particle size (d(p,v) similar to 600 nm) and agglomerated nanoparticle structure also reduced the tracing response time to similar to 5 mu s allowing accurate tracking of turbulent fluctuations approaching 10 kHz. Moreover, no uncertainty arising from multiple scattering effects were observed using ZnO particles in this enclosed wind tunnel geometry at an estimated average seeding density of 2 x 10(11) particles/m(3). Time-average, fluctuation and single-shot temperature-velocity fields are presented for two mainstream turbulence levels ((u) over bar'/(u) over bar (m) = 7% and 14%) and two momentum ratios (IR = 4.7 and 9.3) at a fixed density ratio of 1.55. These flow conditions produce a cooling jet which is detached from the surface. High main flow turbulence causes faster mixing with the surrounding hot gas, increasing the wall-normal spreading of the cooling jet. The instantaneous flow fields show that mainstream turbulence has a significant effect on the shear layer velocity fluctuations and consequently on the streamwise and wall-normal turbulent heat flux, which is derived from the simultaneously acquired temperature-velocity data. We found that high mainstream turbulence reduces the heat flux away from the wall, suggesting that mainstream turbulence can act to diminish cooling performance. Sets of instantaneous measurements recorded at a 6 kHz repetition rate also reveal the dynamic interactions between the main flow turbulence and the cooling jet. These findings and the recorded data can be used to advance turbulence modelling for numerical simulations.
引用
收藏
页数:17
相关论文
共 50 条
  • [21] Estimation of time-resolved turbulent fields through correlation of non-time-resolved field measurements and time-resolved point measurements
    Discetti, Stefano
    Raiola, Marco
    Ianiro, Andrea
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2018, 93 : 119 - 130
  • [22] Development of a Rayleigh scattering diagnostic for time-resolved gas flow velocity, temperature, and density measurements in aerodynamic test facilities
    Mielke, A. F.
    Elam, K. A.
    Sung, C. J.
    2007 22ND INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, 2007, : 163 - +
  • [23] Time resolved velocity and turbulence measurements in turbulent gaseous explosions
    Lindstedt, RP
    Sakthitharan, V
    COMBUSTION AND FLAME, 1998, 114 (3-4) : 469 - 483
  • [24] Effects of Turbulence Promoters of Gas Turbine Blades on Film Cooling Performance
    Agata, Yukiko
    Takahashi, Toshihiko
    Sakai, Eiji
    Nishino, Koichi
    JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2012, 7 (04): : 603 - 618
  • [25] The effects of high mainstream turbulence and turbine vane film cooling on the dispersion of a simulated hot streak
    Jenkins, S
    Varadarajan, K
    Bogard, DG
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2004, 126 (01): : 203 - 211
  • [26] TIME-RESOLVED PROBE MEASUREMENTS IN TRANSIENT GAS DISCHARGES
    ADRIAANS.M
    JOURNAL OF PHYSICS E-SCIENTIFIC INSTRUMENTS, 1973, 6 (08): : 743 - 745
  • [27] TIME-RESOLVED MEASUREMENTS OF SPATIAL VELOCITY DISTRIBUTIONS IN SHOCK EXPERIMENTS
    BARKER, LM
    ASAY, JR
    BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1973, 18 (12): : 1593 - 1593
  • [28] ACCOUNT OF FILM TURBULENCE FOR PREDICTING FILM COOLING EFFECTIVENESS IN GAS-TURBINE COMBUSTORS
    STURGESS, GJ
    JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1980, 102 (03): : 524 - 534
  • [29] Time-resolved gas temperature measurements by laser absorption in a pulsed microwave hydrogen discharge
    Rousseau, A
    Teboul, E
    Sadeghi, N
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2004, 13 (01): : 166 - 176
  • [30] Time-resolved temperature measurements in hypervelocity dust impact
    Collette, A.
    Drake, K.
    Mocker, A.
    Sternovsky, Z.
    Munsat, T.
    Horanyi, M.
    PLANETARY AND SPACE SCIENCE, 2013, 89 : 58 - 62