Optical Diagnostics of Shock-induced Argon Plasmas Based on a Simple Collisional-Radiative Model

Author:

TAKEUCHI Shin1,YAMADA Gouji2,TAKAHASHI Chihiro2,KAWAZOE Hiromitsu1

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Tottori University

2. Department of Mechanical Engineering, Tokai University

Publisher

Japan Society for Aeronautical and Space Sciences

Reference23 articles.

1. 1) Park, C.: Nonequilibrium Hypersonic Aerothermodynamics, John Wiley & Sons, New York, 1990.

2. 2) Gnoffo, P. A., Gupta, R. N. and Shinn, J. L.: Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium, NASA TP-2867, 1989.

3. 3) Gupta, R. N., Yos, J. M., Thompson, R. A., and Lee, K. P.: A Review of Reaction rates and Thermodynamic and Transport Properties for the 11-Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30000 K, NASA TM-101528, 1989.

4. 4) Park, C.: Review of Chemical-Kinetic Problems of Future NASA Missions, I: Earth Entries, Journal of Thermophysics and Heat Transfer, 7, 3 (1993), pp. 385-398.

5. 5) Yamada, G., Takayanagi, H., Suzuki, T. and Fujita, K.: Shock Layer Radiation Analysis using a Hypervelocity Shock Tube (HVST), Transactions of the Japan Society for Aeronautical and Space Sciences, 55, 1 (2012), pp.37-43.

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