Investigation of working processes in a flowing channel of ramjet engine

Chi tiết về thư mục
Parent link:Thermal Science
Vol. 23.— 2019.— [P. 531-536]
Tác giả của công ty: Национальный исследовательский Томский политехнический университет Инженерная школа энергетики Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)
Tác giả khác: Maslov E. A. Evgeny Anatolievich, Faraponov V. V., Arkhipov V. A. Vladimir Afanasjevich, Zharova I. K. Irina Konstantinovna, Kozlov E. A. Evgeny Aleksandrovich, Savkina N. V. Nadezhda Valerjevna
Tóm tắt:Title screen
The technique and results of experimental-theoretical study of gas-dynamics, heat transfer and the structure of gas-flow in the flowing channel of a ramjet engine in Mach number range M = (5-7) are presented. The temperature distribution along the flowing channel of a ramjet engine was experimentally obtained. The temperature along the wall of the flowing channel of the axisymmetric model was measured using the developed thermo-probe. Distributions of Mach number and temperature along the symmetry axis of the flowing channel of the model are obtained numerically. Comparison of the numerical and experimentally obtained values of the Mach number showed their qualitative agreement.
Ngôn ngữ:Tiếng Anh
Được phát hành: 2019
Những chủ đề:
Truy cập trực tuyến:https://doi.org/10.2298/TSCI19S2531M
Định dạng: Điện tử Chương của sách
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=660412

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