Selection of the optimum configuration and calculation studies of the parameters of a cryogenic propulsion system for an unmanned aerial vehicle

Autor: O. V. Tremkina, D. A. Uglanov, V. V. Urlapkin, S. S. Korneev, Yu. V. Komisar

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 20, Iss 4, Pp 59-68 (2022)

A computational study of the parameters of a propulsion system of an unmanned aerial vehicle operating on a cryogenic working medium has been carried out. Liquid nitrogen was selected as the cryogenic working fluid. Two alternative configurations of

Externí odkaz: https://doaj.org/article/35696db3dbed4695a18d5718d103802d

Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines

Autor: M. Hernandez Morales, A. A. Didenko, Yu. V. Komisar, N. I. Gurakov, I. A. Zubrilin, S. G. Matveev, D. V. Yakushkin

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 20, Iss 2, Pp 19-35 (2021)

The paper presents the results of studying the flow characteristics of liquid fuel in pressure jet atomizers of small-sized gas turbine engines with nozzle diameters of 0.4-0.6 mm for various operating and design parameters. The study was carried out

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::aebdf7ebdc800e9b2292167d30dfb70c
https://journals.ssau.ru/vestnik/article/viewFile/8927/8330