OH planar laser-induced fluorescence measurement for H2/O2 jet diffusion flames in rocket combustion condition up to 7.0 MPa-Reference-Cited by-同舟云学术

OH planar laser-induced fluorescence measurement for H₂/O₂ jet diffusion flames in rocket combustion condition up to 7.0 MPa

Published:2019 Issue:2 Volume:14 Page:JTST0018-JTST0018
ISSN:1880-5566
Container-title:Journal of Thermal Science and Technology
language:en
Short-container-title:JTST

Author:

HIGUCHI Yasuhiro¹²,TAKEUCHI Kiyonori¹²,NUNOME Yoshio³,TOMIOKA Sadatake³,SAKAKI Kazuki³,KUDO Taku¹,HAYAKAWA Akihiro¹,KOBAYASHI Hideaki¹

Affiliation:

1. Institute of Fluid Science, Tohoku University

2. Department of Aerospace Engineering, Tohoku University

3. Research and Development Directorate, Japan Aerospace Exploration Agency

Publisher

Japan Society of Mechanical Engineers

Subject

Engineering (miscellaneous),Instrumentation,General Materials Science,Atomic and Molecular Physics, and Optics

Link

https://www.jstage.jst.go.jp/article/jtst/14/2/14_2019jtst0018/_pdf

Reference19 articles.

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3. Gordon, S. and McBride, B. J., Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications (1996), p.1311, NASA Reference Publication.

4. GuoBiao, C., Jian, D., Yang, Z. and Nanjia, Y., Combustion behaviors of GO₂/GH₂ swirl-coaxial injector using non-intrusive optical diagnostics, Actra Astronautica, Vol.123 (2016), pp.246–256.

5. Huynh, H.H., Sweeney, B.A. and Frederick, R.A., Mode assessment of a single element shear-coaxial injector, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (2009), pp.1–21, Paper No. AIAA 2009-5493.

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