Continuum Radiative Flux From Nonisothermal Nongray Atomic Gases
Abstract
The continuum radiative flux from a nonisothermal stagnation shock layer composed of an atomic gas is the subject of this numerical study in which the fluid dynamics and the radiation are assumed to be uncoupled. Consequently, the temperature profile, which is taken to vary linearly through the shock layer, is unperturbed by the radiation. The importance of the ionization edge location and the influence of various spectral shapes of the bound-free radiative cross sections are emphasized. The results are derived by considering ground to free state radiative transitions. The principal of superposition extends the results to multiple electronic state atomic gases. © 1971, American Institute of Aeronautics and Astronautics, Inc., All rights reserved.
Recommended Citation
H. F. Nelson and A. L. Crosbie, "Continuum Radiative Flux From Nonisothermal Nongray Atomic Gases," AIAA Journal, vol. 9, no. 10, pp. 1929 - 1934, American Institute of Aeronautics and Astronautics, Jan 1971.
The definitive version is available at https://doi.org/10.2514/3.50002
Department(s)
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
0001-1452
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2023 American Institute of Aeronautics and Astronautics, All rights reserved.
Publication Date
01 Jan 1971