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Fast pressure-sensitive paint measurements of dynamic stall on a pitching airfoil via intensity- and lifetime-based methods

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Abstract

This study investigated unsteady pressure measurements on a pitching OA309 airfoil at a Mach number of 0.1 using a fast-responding pressure-sensitive paint (fast PSP). Two commonly used data acquisition methods applicable to fast PSPs, namely the real-time intensity-based method and the single-shot lifetime-based method, were separately used to obtain the pressure distributions on the upper surface at a reduced pitching frequency (k = πfc/U∞) of 0.074. The signal-to-noise ratio, influences of model motion, and temperature-induced errors associated with the two methods were compared to explore the advantages and disadvantages of the methods. The real-time intensity-based method outperformed the single-shot lifetime-based method in pressure measurements on moving models with very low speeds. Flow separation and reattachment were identified according to the temporal- and spatial-resolved pressure fields obtained through the real-time intensity-based method; finally, the effects of the pitching amplitude and the leading-edge vortex generators were studied. The results showed that flow separation was postponed as the pitching amplitude increased, while flow reattachment occurred earlier on the airfoil equipped with leading-edge vortex generators.

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References

  • Buchner A, Honnery D, Soria J (2017) Stability and three-dimensional evolution of a transitional dynamic stall vortex. J Fluid Mech 823:166–197

    Article  MathSciNet  Google Scholar 

  • Carr LW (1988) Progress in analysis and prediction of dynamic stall. J Aircr 25(1):6–17

    Article  MathSciNet  Google Scholar 

  • Choudhry A, Leknys R, Arjomandi M et al (2014) An insight into the dynamic stall lift characteristics. Exp Thermal Fluid Sci 58:188–208

    Article  Google Scholar 

  • Costes M, Richez F, Pape A et al (2015) Numerical investigation of three-dimensional effects during dynamic stall. Aerosp Sci Technol 47:216–237

    Article  Google Scholar 

  • Disotell KJ, Nikoueeyan P, Naughton JW et al (2016) Global surface pressure measurements of static and dynamic stall on a wind turbine airfoil at low Reynolds number. Exp Fluids 57:82

    Article  Google Scholar 

  • Fang S, Long SR, Disotell KJ et al (2012) Comparison of unsteady pressure-sensitive paint measurement techniques. AIAA J 50(1):109–122

    Article  Google Scholar 

  • Gardner AD, Klein C, Sachs WE et al (1807) Investigation of three-dimensional dynamic stall on an airfoil using fast-response pressure-sensitive paint. Exp Fluids 2014:55

    Google Scholar 

  • Gordeyev S, Lucca ND, Jumper EJ et al (2014) Comparison of unsteady pressure fields on turrets with different surface features using pressure-sensitive paint. Exp Fluids 55(1):1661

    Article  Google Scholar 

  • Gregory JW, Asai K, Kameda M et al (2008) A review of pressure-sensitive paint for high-speed and unsteady aerodynamics. Proc Instit Mech Eng, Part G: J Aerospace Eng 222(2):249–290

    Article  Google Scholar 

  • Gregory JW, Sakaue H, Liu T et al (2014) Fast pressure-sensitive paint for flow and acoustic diagnostics. Annu Rev Fluid Mech 46(1):303–330

    Article  MathSciNet  Google Scholar 

  • Inoue T, Matsuda Y, Ikami T et al (2021) Data-driven approach for noise reduction in pressure-sensitive paint data based on modal expansion and time-series data at optimally placed points. Phys Fluids 33:077105

    Article  Google Scholar 

  • Juliano TJ, Kumar P, Peng D et al (2011) Single-shot, lifetime-based pressure-sensitive paint for rotating blades. Meas Sci Technol 22(8):085403

    Article  Google Scholar 

  • Kurihara D, Saitoh K, Sakaue H (2020) Uncertainty analysis of motion-capturing pressure-sensitive paint method based on unsteady surface-pressure measurement on fluttering airfoil. Aerosp Sci Technol 103:105878

    Article  Google Scholar 

  • Li Z, Feng L, Karbasian HR et al (2019) Experimental and numerical investigation of three-dimensional vortex structures of a pitching airfoil at a transitional Reynolds number. Chin J Aeronaut 32(10):36–48

    Article  Google Scholar 

  • Liu T, Sullivan JP, Asai K et al (2021) Pressure and temperature sensitive paints, 2nd edn. Springer, Berlin

    Book  Google Scholar 

  • Melius M, Cal RB, Mulleners K (2016) Dynamic stall of an experimental wind turbine blade. Phys Fluids 28(3):034103

    Article  Google Scholar 

  • Mitsuo K, Asai K, Takahashi A et al (2004) Advanced lifetime PSP imaging system for simultaneous pressure and temperature measurement. Meas Sci Technol 17(6):1–11

    Google Scholar 

  • Mulleners K, Raffel M (2012) The onset of dynamic stall revisited. Exp Fluids 52(3):779–793

    Article  Google Scholar 

  • Mulleners K, Raffel M (2013) Dynamic stall development. Exp Fluids 54:1469

    Article  Google Scholar 

  • Pastuhoff M, Yorita D, Asai K et al (2013) Enhancing the signal-to-noise ratio of pressure sensitive paint data by singular value decomposition. Meas Sci Technol 24(7):075301

    Article  Google Scholar 

  • Pastuhoff M, Tillmark N, Alfredsson P (2016) Measuring surface pressure on rotating compressor blades using pressure sensitive paint. Sensors 16(3):344

    Article  Google Scholar 

  • Peng D, Liu Y (2020) Fast Pressure-sensitive paint for understanding complex flows: from regular to harsh environments. Exp Fluids 61(8):1–22

    Google Scholar 

  • Peng D, Wang S, Liu Y (2016) Fast PSP measurements of wall pressure fluctuation in low-speed flows: improvements using proper orthogonal decomposition. Exp Fluids 57(4):45

    Article  Google Scholar 

  • Peng D, Jiao L, Yu Y et al (2017) Single-shot lifetime-based PSP and TSP measurements on turbocharger compressor blades. Exp Fluids 58(9):127

    Article  Google Scholar 

  • Peng D, Gu F, Li Y et al (2018) A novel sprayable fast-responding pressure-sensitive paint based on mesoporous silicone dioxide particles. Sens Actuators, A 279:390–398

    Article  Google Scholar 

  • Sakaue H, Myamoto K, Miyazaki T (2013) A motion-capturing pressure-sensitive paint method. J Appl Phys 113(8):149–156

    Article  Google Scholar 

  • Watkins AN, Leighty BD, Lipford WE et al (2015) Measuring surface pressures on rotor blades using pressure-sensitive paint. AIAA J 54(1):206–215

    Article  Google Scholar 

  • Weiss A, Geisler R, Schwermer T et al (2017) Single-shot pressure-sensitive paint lifetime measurements on fast rotating blades using an optimized double-shutter technique. Exp Fluids 58(9):120

    Article  Google Scholar 

  • Wen X, Liu Y, Li Z et al (2018) Data mining of a clean signal from highly noisy data based on compressed data fusion: a fast-responding pressure-sensitive paint application. Phys Fluids 30(9):097103

    Article  Google Scholar 

  • Wernert P, Geissler W, Raffel M et al (1996) Experimental and numerical investigations of dynamic stall on a pitching airfoil. AIAA J 34(5):982–989

    Article  Google Scholar 

  • Zhao Q, Ma Y, Zhao G (2017) Parametric analyses on dynamic stall control of rotor airfoil via synthetic jet. Chin J Aeronaut 30(6):1818–1834

    Article  Google Scholar 

  • Zhong J, Li J, Guo P et al (2019) Dynamic stall control on a vertical axis wind turbine aerofoil using leading-edge rod. Energy 174:246–260

    Article  Google Scholar 

Download references

Acknowledgements

This work is supported by funding from the National Natural Science Foundation of China (NSFC No. 12102260 & No. 12202476) and the Gas Turbine Research Institute of Shanghai Jiao Tong University.

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Authors and Affiliations

  1. Key Lab of Education Ministry for Power Machinery and Engineering, School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai, 200240, China

    Lingrui Jiao, Xin Wen, Yingzheng Liu & Di Peng

  2. Gas Turbine Research Institute, Shanghai Jiao Tong University, Shanghai, 200240, China

    Lingrui Jiao, Xin Wen, Yingzheng Liu & Di Peng

  3. China Aerodynamic Research and Development Center, Mianyang, 621000, China

    Zheyu Shi, Chunhua Wei & Shuai Ma

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  1. Lingrui Jiao
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  2. Zheyu Shi
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  3. Chunhua Wei
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  4. Shuai Ma
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  5. Xin Wen
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  6. Yingzheng Liu
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  7. Di Peng
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Correspondence to Di Peng.

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Jiao, L., Shi, Z., Wei, C. et al. Fast pressure-sensitive paint measurements of dynamic stall on a pitching airfoil via intensity- and lifetime-based methods. J Vis 27, 333–352 (2024). https://doi.org/10.1007/s12650-024-00973-3

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  • DOI: https://doi.org/10.1007/s12650-024-00973-3

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