A DETAILED UNCERTAINTY ANALYSIS OF ADIABATIC FILM COOLING EFFECTIVENESS MEASUREMENTS USING PRESSURE SENSITIVE PAINT

被引:0
|
作者
Natsui, Greg [1 ]
Little, Zachary [1 ]
Kapat, Jayanta S. [1 ]
Dees, Jason E. [2 ]
Laskowski, Gregory [3 ]
机构
[1] Univ Cent Florida, Lab Turbine Aerodynam Heat Transfer & Durabil, Ctr Adv Turbomachinery & Energy Res, Orlando, FL 32816 USA
[2] GE Global Res, Niskayuna, NY USA
[3] GE Aviat, Lynn, MA USA
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
Pressure sensitive paint (PSP) can be a powerful tool in measuring the adiabatic film cooling effectiveness. There are two distinct sources of error for this measurement technique; the ability to experimentally obtain the data and the validity of the heat and mass transfer analogy for the problem being studied. This paper will assess the experimental aspect of this PSP measurement specifically for film cooling applications. Experiments are conducted in an effort to quantifiably bound expected errors associated with temperature non uniformities in testing and photo-degradation effects. Results show that if careful experimental procedures are put in place, both of these effects can be maintained to have less than 0.022 impact on effectiveness. Through accurate semi-in-situ calibration down to 4% atmospheric pressure, the near-hole distribution of effectiveness is measured with high accuracy. PSP calibrations are performed for multiple coupons, overmultiple days. In addition, to reach a partial pressure of 0 the calibration vessel was purged of all air by flpwing CO2. The primary contribution of this paper lies in the uncertainty analysis performed on the PSP measurement technique. A thorough uncertainty analysis is conducted and described, in order to completely understand the presented measurements and any shortcomings of the PSP technique. This quantification results in larger, albeit more realistic, values of uncertainty, and helps provide a better understanding of film cooling effectiveness measurements taken using the PSP technique. The presented uncertainty analysis takes into account all random error sources associated with sampling and calibration, from intensities to effectiveness. Adiabatic film cooling effectiveness measurements are obtained for a single row of film cooling holes inclined at 20 degrees, with CO2 used as coolant. Data is obtained for six blowing ratios. Maps of uncertainty corresponding to each effectiveness profile are available for each test case. These maps show that the uncertainty varies spatially over the test surface, high effectiveness corresponds to low uncertainty. The noise floors can be as high as 0.04 at effectiveness levels of 0. Day-to-day repeatability is presented for each blowing ratio and shows that laterally averaged effectiveness data is repeatable within 0.02 effectiveness.
引用
收藏
页数:14
相关论文
共 50 条
  • [1] A Detailed Uncertainty Analysis of Adiabatic Film Cooling Effectiveness Measurements Using Pressure-Sensitive Paint
    Natsui, Greg
    Little, Zachary
    Kapat, Jayanta S.
    Dees, Jason E.
    Laskowski, Gregory
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2016, 138 (08):
  • [2] Measurement Uncertainty Analysis in Determining Adiabatic Film Cooling Effectiveness by Using Pressure Sensitive Paint Technique
    Johnson, Blake
    Hu, Hui
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2016, 138 (12):
  • [3] MEASUREMENT UNCERTAINTIES ANALYSIS IN THE DETERMINATION OF ADIABATIC FILM COOLING EFFECTIVENESS BY USING PRESSURE SENSITIVE PAINT (PSP) TECHNIQUE
    Johnson, Blake Everett
    Hu, Hui
    [J]. ASME FLUIDS ENGINEERING DIVISION SUMMER MEETING - 2014, VOL 1D: SYMPOSIA, 2014,
  • [4] A comprehensive deviation analysis of film cooling effectiveness measurements using pressure sensitive paint under various conditions
    Tao, Zhi
    Lou, Yuzhu
    Li, Haiwang
    Zhou, Zhiyu
    Zhang, Jinghan
    Xie, Gang
    [J]. APPLIED THERMAL ENGINEERING, 2024, 236
  • [5] Film-cooling effectiveness on a rotating turbine platform using pressure sensitive paint technique
    Suryanarayanan, A.
    Ozturk, B.
    Schobeiri, M. T.
    Han, J. C.
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2007, VOL 4, PTS A AND B, 2007, : 169 - 183
  • [6] Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique
    Suryanarayanan, A.
    Ozturk, B.
    Schobeiri, M. T.
    Han, J. C.
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2010, 132 (04): : 1 - 13
  • [7] Structure analysis of adiabatic film cooling effectiveness in the near field of a single inclined jet: Measurement using fast-response pressure-sensitive paint
    Khojasteh, Ali Rahimi
    Wang, Shao Fei
    Peng, Di
    Yavuzkurt, Savas
    Liu, Yingzheng
    [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2017, 110 : 629 - 642
  • [8] Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations
    Becchi, R.
    Facchini, B.
    Picchi, A.
    Tarchi, L.
    Coutandin, D.
    Zecchi, S.
    [J]. PROPULSION AND POWER RESEARCH, 2015, 4 (04) : 190 - 201
  • [9] Film cooling effectiveness on the leading edge of a rotating film-cooled blade using pressure sensitive paint
    Ahn, Jaeyong
    Schobeiri, M. T.
    Han, Je-Chin
    Moon, Hee-Koo
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2005, VOL 3 PTS A AND B, 2005, : 375 - 384
  • [10] Unsteady analysis of adiabatic film cooling effectiveness behind circular, shaped, and sand-dune-inspired film cooling holes: Measurement using fast-response pressure-sensitive paint
    Zhou, Wenwu
    Peng, Di
    Wen, Xin
    Liu, Yingzheng
    Hu, Hui
    [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2018, 125 : 1003 - 1016