Temperature Measurement of HEK-X Expansion Tube Flow by Laser Absorption Spectroscopy
Author:
Affiliation:
1. Department of Engineering, Shizuoka University
2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
3. Kakuda Space Center, Japan Aerospace Exploration Agency
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/64/3/64_T-20-38/_pdf
Reference6 articles.
1. 1) Lu, F. K. and Marren, D. E.: Advanced Hypersonic Test Facilities, AIAA, Virginia, 2002, pp. 205–352.
2. 2) Tanno, H., Komuro, T., Sato, K., Itoh, K., Arai, K., and Yamada, K.: Basic Characteristics of the Free-Piston Driven Expansion Tube JAXA HEK-X, AIAA Paper 2016-3817, 2016.
3. 3) Yamada, T.: Numerical Analysis of CO2 Expansion Tube Flows with Thermochemical Nonequilibrium, Master Thesis, Shizuoka University, 2017.
4. 4) Matsui, M., Komurasaki, K., Herdrich, G., and Auweter-Kurtz, M.: Enthalpy Measurement in Inductively Heated Plasma Generator Flow by Laser Absorption Spectroscopy, AIAA J., 43 (2005), pp. 2060–2064.
5. 5) Matsui, M., Tanaka, K., Nomura, S., Komurasaki, K., Yamagiwa, Y., and Arakawa, Y.: Generation and Diagnostics of Atmospheric Pressure CO2 Plasma by Laser Driven Plasma Wind Tunnel, J. Appl. Phys., 112 (2012), 033301.
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