Расчетно-теоретическое исследование взаимодействия высокотемпературного сверхзвукового потока с моделью летательного аппарата

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Д.М. Ягодников, Н.И. Быков, В.И. Томак, А.С. Бурков, Н.Я. Ирьянов
12 Инженерный журнал: наука и инновации # 12016
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Yagodnikov D.A., Dr. Sci. (Eng.), Professor, Head of the Department of Rocket Engines,
Bauman Moscow State Technical University. Author of over 220 scientific works in the
field of experimental and theoretical research of working processes and development of
contactless methods of rocket and jet engines diagnostics. e-mail:
Bykov N.I. (b.1990) graduated from Bauman Moscow State Technical University in
2013. Design engineer, S.P. Korolev Rocket and Space Corporation “Energia”. Author of
6 scientific works in the fields of rocket engine analysis by the techniques of
computational fluid dynamics (CFD) and working process research in power stations
based on powdered aluminum. e-mail:
Tomak V.I. (b.1946) graduated from Bauman Moscow State Technical University in
1970. Cand. Sci. (Eng.), Head of Department, Research Institute of Power Engineering,
Bauman Moscow State Technical University. Author of over 10 inventions, patents and
20 scientific works. Expert in the fields of rocket and jet engine experimental
development and construction materials for rocket and space equipment.
e-mail:
Burkov A.S., Post-graduate student, Bauman Moscow State Technical University.
Co-author of 10 publications on pilot studies of construction material characteristics and
contactless diagnostics of high-temperature flows. Expert in the field of developmental
testing of rocket and jet engines. e-mail:
Iryanov . (b. 1938) graduated from Bauman Moscow State Technical University in
1961. Cand. Sci. (Eng.), Associate Professor, Department of Rocket Engines, Bauman
Moscow State Technical University. Author of over 40 scientific works in the fields of
two-phase flow in rocket engine gas circuits and methodology of rocket engines
development. e-mail: