Determination of the Electron Temperature of Shock-Heated Air from the Measured Radiation Intensities

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Abstract

The results of the radiation characteristics of shock-heated air measurements in the vacuum-ultraviolet region are presented. The experiments are carried out in the STS shock tube of the Institute of Mechanics, Moscow State University at shock-wave velocities of 7.3 to 10.7 km/s and initial pressures in the low-pressure chamber of 0.125, 0.2, and 0.25 Torr. An analytical model of the radiation process is constructed, which takes into account the absorption of radiation during its passage through the air . Processing the experimental dependences of the radiation intensity on time for the main radiation lines using this model made it possible to propose a radiation method for determining the electron temperature of a shock-heated gas. The presented data are compared with the experimental data of other authors.

About the authors

N. G. Bykova

Institute of Mechanics, Moscow State University

Email: vyl69@mail.ru
Moscow, Russia

I. E. Zabelinskii

Institute of Mechanics, Moscow State University

Email: vyl69@mail.ru
Moscow, Russia

P. V. Kozlov

Institute of Mechanics, Moscow State University

Email: vyl69@mail.ru
Moscow, Russia

G. Ya. Gerasimov

Institute of Mechanics, Moscow State University

Email: vyl69@mail.ru
Moscow, Russia

V. Yu. Levashov

Institute of Mechanics, Moscow State University

Author for correspondence.
Email: vyl69@mail.ru
Moscow, Russia

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Copyright (c) 2023 Н.Г. Быкова, И.Е. Забелинский, П.В. Козлов, Г.Я. Герасимов, В.Ю. Левашов