Velocity Parameter Generalization of Ideally Dissociated Gas Recombination
Zbornik radova, Tome 3 (1979) no. 11, p. 102
Voir la notice de l'article provenant de la source eLibrary of Mathematical Institute of the Serbian Academy of Sciences and Arts
In this work it is discussed about а laminar boundary layer оп the body of
an arbitrary form, which moves at supersonic speed through the earth atmosphere,
e.g. supersonic planes, rockets, space ships, Such high speeds lead to the so-called
supersonic warming of the aircraft caused Ьу an intensive transition ofthe mechanical
energy into the thermal one, in the impact wave itself, which is formed in front
of the aircraft, as well as in the thin layer next to its surface and it happens оп
account of the force of friction. Вecause of that high temperature are developed in
the space of flow close to the aircaft surface which lead to thermochemical reactions
of dissociation and recombination, that is they change the "homogeneous"
air into а multicomponent mixture of gases: 02, О, N2, N, NO and Аг. It is to
Ье remarked that the former thermochemical reactions are followed Ьу the process
of diffusion, whereat it is possible that the material of the overflowed aircraft
surface enters the chemical reactions with the mentioned component of the mixture.
@article{ZR_1979_3_11_a10,
author = {Branko R. Obrovi\'c},
title = {Velocity {Parameter} {Generalization} of {Ideally} {Dissociated} {Gas} {Recombination}},
journal = {Zbornik radova},
pages = {102 },
publisher = {mathdoc},
volume = {3},
number = {11},
year = {1979},
language = {en},
url = {http://geodesic.mathdoc.fr/item/ZR_1979_3_11_a10/}
}
Branko R. Obrović. Velocity Parameter Generalization of Ideally Dissociated Gas Recombination. Zbornik radova, Tome 3 (1979) no. 11, p. 102 . http://geodesic.mathdoc.fr/item/ZR_1979_3_11_a10/