Analysis of VUV radiation measurements from high temperature air mixtures

Author:

Lemal Adrien1,Nishimura Sayaka2,Nomura Satoshi1,Takayanagi Hiroki1,Matsuyama Shingo1,Fujita Kazuhisa1

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. Shizuoka University

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. Radiative Heating Uncertainty for Hyperbolic Earth Entry, Part 1: Flight Simulation Modeling and Uncertainty

2. A. Lemal, Prediction of nonequilibrium air plasma radiation behind a shock wave with a collisional-radiative model: application to shock-tube experiments representative of Earth reentry, Ph.D thesis,Ecole Centrale Paris, 2013.

3. Development of Shock Tube for Ground Testing Reentry Aerothermodynamics

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1. VUV to IR Emission Spectroscopy and Interferometry Diagnostics for the European Shock Tube for High-Enthalpy Research;Sensors;2023-06-29

2. Nonequilibrium Effects in Precursor Electrons Ahead of Shock Waves;Journal of Thermophysics and Heat Transfer;2021-07

3. Numerical investigation of a hypersonic flow around a capsule in CO2–N2 environment;European Journal of Mechanics - B/Fluids;2020-03

4. Analysis of Shockwave Radiation Data in Nitrogen;AIAA Aviation 2019 Forum;2019-06-15

5. Simulation of Ionization and Electronic Excitationin Hypersonic Shock Tube Flows Using DSMC;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2018

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