The brief introduction of different laser diagnostics methods used in aeroengine combustion research

Article


Xing, Fei, Zhao, Mengmeng and Zhao, Jian. 2016. "The brief introduction of different laser diagnostics methods used in aeroengine combustion research." Journal of Sensors. 2016, pp. 1-13. https://doi.org/10.1155/2016/2183569
Article Title

The brief introduction of different laser diagnostics methods used in aeroengine combustion research

ERA Journal ID201141
Article CategoryArticle
AuthorsXing, Fei (Author), Zhao, Mengmeng (Author) and Zhao, Jian (Author)
Journal TitleJournal of Sensors
Journal Citation2016, pp. 1-13
Article Number2183569
Number of Pages13
Year2016
Place of PublicationUnited States
ISSN1687-725X
1687-7268
Digital Object Identifier (DOI)https://doi.org/10.1155/2016/2183569
Web Address (URL)http://www.hindawi.com/journals/js/2016/2183569/
Abstract

Combustion test diagnosis has always been one of the most important technologies for the development of aerospace engineering. The traditional methods of measurement have been unable to meet the requirements of accurate capture of the flow field in the development process of the aeroengine combustor. Therefore, the development of high-precision measurement and diagnostic techniques to meet the needs of the aeroengine combustor design is imperative. Laser diagnostics techniques developed quickly in the past several years. They are used to measure the parameters of the combustion flow field such as velocity, temperature, and
components concentration with high space and time resolution and brought no disturbance. Planar laser-induced fluorescence, coherent anti-Stokes Raman scattering, tunable diode laser absorption spectroscopy, and Raman scattering were introduced systemically in this paper. After analysis of their own advantages and disadvantages, the authors considered validated Raman scattering system and Tunable Diode Laser Absorption Tomography are more suitable for research activities on aeroengine combustion systems.

KeywordsAeroengine combustors; Coherent anti Stokes Raman scattering; Diagnostics techniques; High-precision measurement; Methods of measurement; Planar laser induced fluorescence; Tunable diode laser absorption; Tunable diode laser absorption spectroscopy
ANZSRC Field of Research 2020401201. Aerodynamics (excl. hypersonic aerodynamics)
400106. Hypersonic propulsion and hypersonic aerothermodynamics
Byline AffiliationsXiamen University, China
School of Mechanical and Electrical Engineering
Changcheng Institute of Metrology and Measurement, China
Institution of OriginUniversity of Southern Queensland
Permalink -

https://research.usq.edu.au/item/q374y/the-brief-introduction-of-different-laser-diagnostics-methods-used-in-aeroengine-combustion-research

  • 1797
    total views
  • 187
    total downloads
  • 2
    views this month
  • 1
    downloads this month

Export as

Related outputs

Supersonic combustion of hydrogen in Mach 2 flows over an axisymmetric model
Zhao, Mengmeng, Buttsworth, David and Choudhury, Rishabh. 2018. "Supersonic combustion of hydrogen in Mach 2 flows over an axisymmetric model." 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference (AIAA 2018). Orlando, United States 17 - 19 Sep 2018 United States. https://doi.org/10.2514/6.2018-5252
Experimental and numerical study of OH* chemiluminescence in hydrogen diffusion flames
Zhao, Mengmeng, Buttsworth, David and Choudhury, Rishabh. 2018. "Experimental and numerical study of OH* chemiluminescence in hydrogen diffusion flames." Combustion and Flame. 197, pp. 369-377. https://doi.org/10.1016/j.combustflame.2018.08.019
Study of an axisymmetric backward facing step model in a supersonic flow
Zhao, Mengmeng, Buttsworth, David R., Choudhury, Rishabh, Malpress, Ray and Xing, Fei. 2016. "Study of an axisymmetric backward facing step model in a supersonic flow." 21st AIAA International Space Planes and Hypersonics Technologies Conference (Hypersonics 2017). Xiamen, China 06 - 09 Mar 2017 United States. https://doi.org/10.2514/6.2017-2181
Effect of impingement/effusion hole-area ratio on discharge coefficients of double cooling wall
Zhang, Chi, Xu, Quanhong, Zhao, Mengmeng, Lin, Yuzhen and Liu, Gaoen. 2006. "Effect of impingement/effusion hole-area ratio on discharge coefficients of double cooling wall." ASME Turbo Expo 2006. Barcelona, Spain 08 - 11 May 2006 United States. https://doi.org/10.1115/GT2006-90612
Effect of inclined angle on discharge coefficient of the discrete holes in curved wall
Zhang, Chi, Zhao, Mengmeng, Lin, Yu-zhen and Liu, Gao-en. 2007. "Effect of inclined angle on discharge coefficient of the discrete holes in curved wall." Journal of Aerospace Power. 22 (7), pp. 1127-1131.
Study of overall cooling effectiveness of discrete holes with different angles to concave wall
Zhao, Mengmeng, Zhang, Chi, Lin, Yu-zhen and Liu, Gao-en. 2007. "Study of overall cooling effectiveness of discrete holes with different angles to concave wall." Journal of Aerospace Power. 22 (2), pp. 210-215.
Absolute concentration measurements of OH* in an axisymmetric hydrogen-air premixed flame adjacent to a hot graphite model
Zhao, M. M., Choudhury, R., Malpress, R. and Buttsworth, D. R.. 2016. "Absolute concentration measurements of OH* in an axisymmetric hydrogen-air premixed flame adjacent to a hot graphite model." 20th Australasian Fluid Mechanics Conference (AFMC 2016). Perth, Australia 05 - 08 Dec 2016 Australia.
Simulations of a cavity based two-dimensional scramjet model
Xing, F., Zhao, M. and Zhang, S.. 2012. "Simulations of a cavity based two-dimensional scramjet model." Brandner, P. A. and Pearce, B. W. (ed.) 18th Australasian Fluid Mechanics Conference (AFMC 2012). Launceston, Australia 03 - 07 Dec 2012
Experimental investigation of airflow distribution for a novel combustor mode
Li, Qiong, Zhao, Mengmeng and Xing, Fei. 2013. "Experimental investigation of airflow distribution for a novel combustor mode." Applied Mechanics and Materials. 284-287, pp. 743-747. https://doi.org/10.4028/www.scientific.net/AMM.284-287.743
External hot surface axisymmetric models for supersonic combustion
Zhao, Mengmeng. 2016. External hot surface axisymmetric models for supersonic combustion. PhD Thesis Doctor of Philosophy. University of Southern Queensland. https://doi.org/10.26192/5bf61fcbbc4a1