Skip to main content
Log in

Study of density field measurement based on NPLS technique in supersonic flow

  • Published:
Science in China Series G: Physics, Mechanics and Astronomy Aims and scope Submit manuscript

Abstract

Due to the influence of shock wave and turbulence, supersonic density field exhibits strongly inhomogeneous and unsteady characteristics. Applying traditional density field measurement techniques to supersonic flows yields three problems: low spatiotemporal resolution, limitation of measuring 3D density field, and low signal to noise ratio (SNR). A new method based on Nano-based Planar Laser Scattering (NPLS) technique is proposed in this paper to measure supersonic density field. This method measures planar transient density field in 3D supersonic flow by calibrating the relationship between density and concentration of tracer particles, which would display the density fluctuation due to the influence of shock waves and vortexes. The application of this new method to density field measurement of supersonic optical bow cap is introduced in this paper, and the results reveal shock wave, turbulent boundary layer in the flow with the spatial resolution of 93.2 μm/pixel. By analyzing the results at interval of 5 μs, temporal evolution of density field can be observed.

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.

Similar content being viewed by others

References

  1. Fan J C. Modern Flow Visualization. Beijing: National Defense Industry Press, 2002

    Google Scholar 

  2. Zhang B, Song Y, Song Y Z, et al. A new reconstruction algorithm for Moiré tomography in the measurements of complex density distributions. J Optoelectr Laser, 2007, 18(2): 224–227

    Google Scholar 

  3. Yi S H, Chang X Y. Interferometry measurement of density field and the calculation of strip processing. Fire Safety Sci, 2000, 9(1): 39–43

    Google Scholar 

  4. Guo L D, Yang H, Zeng X J. Laser holographic interferometer measurement to high speed and supersonic axial symmetric model. Exp Meas Fluid Mech, 2000, 14(2): 77–82

    Google Scholar 

  5. Hashimoto T, Naitou K, Takayama K. Density measurement over a sphere in free piston shock tunnel. In: Proceedings of the AIAA/NALNASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, April 24–27, 2001

  6. Nonaka S, Mizuno H, Hashimoto T, et al. Density measurement over a sphere in ballistic range. In: Proceedings of the 38th Aerospace Sciences Meeting & Exhibit, Reno, NEVADA, January 10–13, 2000

  7. Meier G E A. New optical tools for fluid mechanics. In: Proceedings of the 8th International Symposium Flow Visualization, Sorrento, Italy, September 1–4, 1998

  8. Venkatakrishnan L, Meier G E A. Density measurement using the background oriented schlieren technique. Exp Fluids, 2004, 37: 237–247

    Article  Google Scholar 

  9. Sourgen F, Haertig J, George A, et al. Validation of CFD density field in supersonic axisymmetric flows using BOS and differential interferometry. In: Proceedings of AIAA Atmospheric Flight Mechanics Conference and Exhibit, San Francisco, California, August 15–18, 2005

  10. Danehy P M, O’Byrne S. Measurement of NO density in a free-piston shock tunnel using PLIF. In: Proceedings of the 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NEVADA, January 11–14, 1999

  11. Geng H, Zhai Z C, Zhou S B, et al. Investigation of the density flow field of underexpanded free jet with acetone planar laser induced fluorescence. J Exp Fluid Mech, 2006, 20(3): 85–90

    Google Scholar 

  12. Elliott G S, Boguszko M, Carter C. Filtered Rayleigh scattering: Toward multiple property measurements. In: Proceedings of the 39th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NEVADA, January 8–11, 2001

  13. Panda J, Seasholtz R G. Density fluctuation measurement in supersonic fully expanded jets using Rayleigh scattering. AIAA 99-1870

  14. Panda J, Seasholtz R G. Density measurement in underexpanded supersonic jets using Rayleigh scattering. In: Proceeding of the 36th Aerospace Sciences Meeting & Exhibit, Reno, NEVADA, January 12–15, 1998

  15. Mielke A F, Elam K A, Sung C J. Rayleigh scattering diagnostic for measurement of temperature, velocity, and density fluctuation spectra. In: Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 9–12, 2006

  16. Wang J, Yao J Q, Yu Y Z, et al. Instantaneous two-dimensional density measurements of gas flow by Rayleigh scattering. J Optoelectr Laser, 2001, 12(1): 62–64

    Google Scholar 

  17. Zhao Y X. Experimental investigation of spatiotemporal structures of supersonic mixing layer. Doctor Dissertation. Changsha: National University of Defense Technology, 2008

    Google Scholar 

  18. Zhao Y X, Yi S H, Tian L F, et al. The fractal measurement of experimental images of supersonic turbulent mixing layer. Sci China Ser G-Phys Mech Astron, 2008, 52(2): 140–143

    Article  ADS  Google Scholar 

  19. Zheng J, Xu C G, Xiao D G, et al. The technique of digit image’s illumination uneven elimination. Trans Beijing Inst Technol, 2003, 23(3): 285–289

    Google Scholar 

  20. Smith W J. Modern Optical Engineering: The Design Of Optical Systems. 2nd ed. New York: McGraw-Hill Press, 1990

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to LiFeng Tian.

Additional information

Supported by the National Natural Science Foundation of China (Grant No. 10672178)

Rights and permissions

Reprints and permissions

About this article

Cite this article

Tian, L., Yi, S., Zhao, Y. et al. Study of density field measurement based on NPLS technique in supersonic flow. Sci. China Ser. G-Phys. Mech. Astron. 52, 1357–1363 (2009). https://doi.org/10.1007/s11433-009-0180-4

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11433-009-0180-4

Keywords

Navigation