Skip to main content

Advertisement

Log in

Detection of small-amplitude periodic surface pressure fluctuation by pressure-sensitive paint measurements using frequency-domain methods

  • Research Article
  • Published:
Experiments in Fluids Aims and scope Submit manuscript

Abstract

Image measurement using pressure-sensitive paint (PSP) is an effective tool for analyzing the unsteady pressure field on the surface of a body in a low-speed air flow, which is associated with wind noise. In this study, the surface pressure fluctuation due to the tonal trailing edge (TE) noise for a two-dimensional NACA 0012 airfoil was quantitatively detected using a porous anodized aluminum PSP (AA-PSP). The emission from the PSP upon illumination by a blue laser diode was captured using a 12-bit high-speed complementary metal-oxide-semiconductor (CMOS) camera. The intensities of the captured images were converted to pressures using a standard intensity-based method. Three image-processing methods based on the fast Fourier transform (FFT) were tested to determine their efficiency in improving the signal-to-noise ratio (SNR) of the unsteady PSP data. In addition to two fundamental FFT techniques (the full data and ensemble averaging FFTs), a technique using the coherent output power (COP), which involves the cross correlation between the PSP data and the signal measured using a pointwise sound-level meter, was tested. Preliminary tests indicated that random photon shot noise dominates the intensity fluctuations in the captured PSP emissions above 200 Hz. Pressure fluctuations associated with the TE noise, whose dominant frequency is approximately 940 Hz, were successfully measured by analyzing 40,960 sequential PSP images recorded at 10 kfps. Quantitative validation using the power spectrum indicates that the COP technique is the most effective method of identification of the pressure fluctuation directly related to TE noise. It is possible to distinguish power differences with a resolution of 10 Pa\(^2\) (4 Pa in amplitude) when the COP was employed without use of another wind-off data. This resolution cannot be achieved by the ensemble averaging FFT because of an insufficient elimination of the background noise.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13

Similar content being viewed by others

References

  • Ali MY, Pandey A, Gregory JW (2016) Dynamic mode decomposition of fast pressure sensitive paint data. Sensors 16:862. https://doi.org/10.3390/s16060862

    Article  Google Scholar 

  • Asai K, Yorita D (2011) Unsteady PSP measurement in low-speed flow – Overview of recent advancement at Tohoku University. In: Proceeding of the 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA 2011-847. https://doi.org/10.2514/6.2011-847

  • Bell JH, Schairer ET, Hand LA, Mehta RD (2001) Surface pressure measurements using luminescent coatings. Annu Rev Fluid Mech 33:155–206

    Article  MATH  Google Scholar 

  • Bendat JS, Piersol AG (1980) Engineering applications of correlation and spectral analysis. Wiley, New York

    MATH  Google Scholar 

  • Desquesnes G, Terracol M, Sagaut P (2007) Numerical investigation of the tone noise mechanism over laminar airfoils. J Fluid Mech 591:155–182

    Article  MATH  Google Scholar 

  • Doolan CJ, Moreau DJ (2016) Flow-induced noise generated by sub-boundary layer steps. Exp Therm Fluid Sci 72:47–58

    Article  Google Scholar 

  • Gabriel C, Müller S, Ullrich F, Lerch R (2014) A new kind of sensor array for measuring spatial coherence of surface pressure on a car’s side window. J Sound Vib 333:901–915. https://doi.org/10.1016/j.jsv.2013.09.045

    Article  Google Scholar 

  • Gade S, Hald J (2012) Noise source identification with increased spatial resolution in automotive industry. J Acoust Soc Am 131:3220. https://doi.org/10.1121/1.4708008

    Article  Google Scholar 

  • Goldman S (1999) Vibration spectrum analysis: a practical approach, 2nd edn. Industrial Press, New York

    Google Scholar 

  • Gregory JW, Asai K, Kameda M, Liu T, Sullivan JP (2008) A review of pressure-sensitive paint for high-speed and unsteady aerodynamics. J Aerosp Eng 222:249–290. https://doi.org/10.1243/09544100JAERO243

    Google Scholar 

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

    Article  MathSciNet  MATH  Google Scholar 

  • Hutcheson FV, Brooks TF (2002) Measurement of trailing edge noise using directional array and coherent output power methods. In: Proceedings of the 8th AIAA/CEAS Aeroacoustics Conference, AIAA-2002-2472. https://doi.org/10.2514/6.2002-2472

  • Kameda M, Tezuka N, Hangai T, Asai K, Nakakita K, Amao Y (2004) Adsorptive pressure-sensitive coatings on porous anodized aluminum. Meas Sci Technol 15:489–500

    Article  Google Scholar 

  • Kameda M, Tabei T, Nakakita K, Sakaue H, Asai K (2005) Image measurements of unsteady pressure fluctuation by a pressure-sensitive coating on porous anodized aluminum. Meas Sci Technol 16:2517–2524

    Article  Google Scholar 

  • Kameda M, Yoshida M, Sekiya T, Nakakita K (2015) Humidity effects in the response of a porous pressure-sensitive paint. Sens Actuators B Chem 208:399–405

    Article  Google Scholar 

  • Kido K (2015) Digital fourier analysis: fundamentals. Springer, New York

    MATH  Google Scholar 

  • Krause J, Gallman JM, Moeller MJ, White RD (2014) A microphone array on a chip for high spatial resolution measurements of turbulence. IEEE J Microelectrochem Syst 23:1164–1181. https://doi.org/10.1109/JMEMS.2014.2307556

    Article  Google Scholar 

  • Liu T, Sullivan JP (2005) Pressure and temperature sensitive paints. Springer, Berlin

    Google Scholar 

  • Marple SL (1987) Digital spectral analysis with applications. Prentice-Hall, New Jersey

    Google Scholar 

  • McAlpine A, Nash E, Lowson M (1999) On the generation of discrete frequency tones by the flow around an aerofoil. J Sound Vib 222:753–779

    Article  Google Scholar 

  • Mérienne M-C, Molton P, Bur R, Le Sant Y (2015) Pressure-sensitive paint application to an oscillating shock wave in a transonic flow. AIAA J 53:3208–3220. https://doi.org/10.2514/1.J053744

    Article  Google Scholar 

  • Nakakita K (2011) Unsteady pressure measurement on NACA0012 model using global low-speed unsteady PSP technique. In: Proceedings of the 41st AIAA Fluid Dynamics Conference and Exhibit, AIAA 2011-3901. https://doi.org/10.2514/6.2011-3901

  • Nakakita K (2013) Phase delay and correlation area detection of unsteady pressure field using unsteady PSP measurement. In: Proceedings of AIAA Ground Testing Conference, AIAA 2013–3124: https://doi.org/10.2514/6.2013-3124

  • Nash E, Lowson M, McAlpine A (1999) Boundary layer instability noise on aerofoils. J Fluid Mech 382:27–61

    Article  MATH  Google Scholar 

  • Pastuhoff M, Yorita D, Asai K, Alfredsson PH (2013) Enhancing the signal-to-noise ratio of pressure sensitive paint data by singular value decomposition. Meas Sci Technol 24:075301. https://doi.org/10.1088/0957-0233/24/7/075301

    Article  Google Scholar 

  • Peng D, Jiao L, Sun Z, Gu Y, Liu Y (2016a) Simultaneous PSP and TSP measurements of transient flow in a long-duration hypersonic tunnel. Exp Fluids 57:188

    Article  Google Scholar 

  • Peng D, Wang S, Liu Y (2016b) Fast PSP measurements of wall pressure fluctuation in low speed flows: improvements using proper orthogonal decomposition. Exp Fluids 57:45. https://doi.org/10.1007/s00348-016-2130-z

    Article  Google Scholar 

  • Piet J-F, Elias G, Lebigot P (1999) Localization of acoustic source from a landing air-craft with a microphone array. In: Proceedings of 5th AIAA/CEAS Aeroacoustics Conference and Exhibit, Aeroacoustics Conferences, AIAA-1999-1811. https://doi.org/10.2514/6.1999-1811

  • Plogmann B, Herrig A, Würz W (2013) Experimental investigations of a trailing edge noise feedback mechanism on a NACA 0012 airfoil. Exp Fluids 54:1480

    Article  Google Scholar 

  • Sakaue H, Tabei T, Kameda M (2006) Hydrophobic monolayer coating on anodized aluminum pressure-sensitive paint. Sens Actuators B Chem 119:504–511

    Article  Google Scholar 

  • Siller HA (2012) Localisation of sound sources on aircraft in flight. In: Proceedings of ASME 2012 Noise Control and Acoustics Division Conference at InterNoise 2012, Paper No. NCAD2012-0575, pp. 193-202; 10 pages. https://doi.org/10.1115/NCAD2012-0575

  • Yorita D, Nagai H, Asai K, Narumi T (2010) Unsteady PSP technique for measuring naturally-disturbed periodic phenomena. In: Proceedings of the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA 2010-307. https://doi.org/10.2514/6.2010-307

Download references

Acknowledgements

This work was financially supported by JSPS KAKENHI under Grant numbers 2528929 and 16H04265.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Masaharu Kameda.

Additional information

Publisher's Note

Publisher's Note Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Noda, T., Nakakita, K., Wakahara, M. et al. Detection of small-amplitude periodic surface pressure fluctuation by pressure-sensitive paint measurements using frequency-domain methods. Exp Fluids 59, 94 (2018). https://doi.org/10.1007/s00348-018-2550-z

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • DOI: https://doi.org/10.1007/s00348-018-2550-z

Navigation