Abstract
Results are presented of experimental disintegration by a high-enthalpy gas stream of models made of asbestos material and graphite. The high-temperature aerodynamic shock-layer heating was modeled using an electrodeless plasma generator, which allowed the thermal boundary layer to be studied on the disintegrating models under convective and radiative heating conditions. The profiles of rotational and vibrational temperature in the multicomponent boundary layer, measured using the CN molecule, coincided.
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E. B. Georg, Yu. K. Rulev, and M. I. Yakushin, “Investigation of the heat flux at the forward stagnation point of bodies in a low-temperature subsonic stream,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 5 (1973).
V. A. Kamenshchikov, Yu. A. Plastinin, V. M. Nikolaev, and L. A. Novitskii, Radiative Properties of Gases at High Temperatures [in Russian], Mashinostroenie, Moscow (1971).
S. S. Penner, Quantitative Molecular Spectroscopy and Gas Emissivities, Pergamon (1962).
H. P. Knauss and M. S. McCay, “Temperature determinations from band spectral data,” Phys. Rev., 52, No. 11 (1937).
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 26–31, January–February, 1976.
The authors thank N. A. Generalov for his interest in the work and for fruitful discussions.
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Georg, É.B., Yakushin, M.I. Thermal boundary layer on models disintegrating in a high-enthalpy gas stream. Fluid Dyn 11, 21–27 (1976). https://doi.org/10.1007/BF01023390
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DOI: https://doi.org/10.1007/BF01023390