Quantitative Schlieren and its Applications as a Measurement Method in the Energy-Based Industry

Authors

  • Emilia Prisacariu Politechnica University of Bucharest
  • Marius Stefan Enache Politechnica University of Bucharest

Abstract

Quantitative Schlieren is a relatively underexplored measurement technique. Although the Schlieren method has been established since the mid-20th century, its quantitative advantages have become more apparent with advancements in image post-processing. This post-processing generates a density map that can be converted into maps for temperature and pressure specific to the observed phenomena. Because the method is non-intrusive, it requires minimal auxiliary equipment—such as cables or transducers—and eliminates the need for consumables typically associated with pressure probe calibration. The non-intrusive nature of the method minimizes measurement errors, as it does not disrupt the flow where pressure probes are used, and relies solely on optical equipment, which is versatile for various experimental setups. This presents an entrepreneurial opportunity to develop a wind tunnel for pressure probe calibration, allowing for the design and calibration of probes with specific geometries. Such an innovation would contribute to a more environmentally friendly industry and position Romania among European nations capable of sustainable pressure probe production and calibration.

References

Adrian, R. J., & Yao, J. (2004). Particle Image Velocimetry: A review of the theory and applications. Measurement Science and Technology, 15(6), pp. 1442-1467.

Kumar, N. A. K. M., & Clarke, S. A. G. W. (2005). Schlieren and shadowgraphy: An introduction to the techniques. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 219(7), 743-757

Li, B. C. L. R., & Wong, A. G. H. (2017). Application of Schlieren technique for the study of combustion phenomena. Applied Thermal Engineering, 113, 104-114.

Marth, L. C. P. M., Stulz, S. W. L., & Sayers, M. W. B. (2000). Laser-Induced Fluorescence for gas temperature measurements: A review. Journal of Quantitative Spectroscopy and Radiative Transfer, 65(1), pp.1-30.

O'Brien, G. F., Smith, L. M., & Jones, K. H. (2011). Visualization of combustion processes using Schlieren imaging. Journal of Propulsion and Power, 27(6), 1290-1299.

Pan, T., & S. L. H. (2014). Experimental analysis of a horizontal-axis wind turbine with swept blades using PIV data. Journal of Wind Engineering and Industrial Aerodynamics, 126, 67-76.

Online Sources

NASA Langley Research Center. (n.d.). Supersonic tunnel. Online. URL: https://www.nasa.gov/centers/langley/

German-Dutch Wind Tunnel. (n.d.). German-Dutch wind tunnel. Online. URL: http://www.dnw.aero/

Beckman Institute for Advanced Science and Technology. (n.d.). Beckman Institute Wind Tunnel. Online. URL: from https://beckman.illinois.edu/.

ONERA & DLR. (n.d.). French-German Wind Tunnel. Online. URL: https://www.onera.fr/en and https://www.dlr.de.

Institute of Aerodynamics and Gas Dynamics, University of Stuttgart. (n.d.). Institute of Aerodynamics and Gas Dynamics. Online. URL: https://www.iag.uni-stuttgart.de/en/.

Downloads

Published

2021-06-30

Issue

Section

Miscellaneous