Investigation of working processes in a flowing channel of ramjet engine
| Parent link: | Thermal Science Vol. 23.— 2019.— [P. 531-536] |
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| Körperschaft: | |
| Weitere Verfasser: | , , , , , |
| Zusammenfassung: | 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. |
| Sprache: | Englisch |
| Veröffentlicht: |
2019
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| Schlagworte: | |
| Online-Zugang: | https://doi.org/10.2298/TSCI19S2531M |
| Format: | Elektronisch Buchkapitel |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=660412 |
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| 200 | 1 | |a Investigation of working processes in a flowing channel of ramjet engine |f E. A. Maslov [et al.] | |
| 203 | |a Text |c electronic | ||
| 300 | |a Title screen | ||
| 320 | |a [References: 11 tit.] | ||
| 330 | |a 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. | ||
| 461 | |t Thermal Science | ||
| 463 | |t Vol. 23 |v [P. 531-536] |d 2019 | ||
| 610 | 1 | |a электронный ресурс | |
| 610 | 1 | |a труды учёных ТПУ | |
| 610 | 1 | |a gas dynamics | |
| 610 | 1 | |a heat transfer | |
| 610 | 1 | |a supersonic flow | |
| 610 | 1 | |a experimental research | |
| 610 | 1 | |a mathematical modeling | |
| 610 | 1 | |a газовая динамика | |
| 610 | 1 | |a теплообмен | |
| 610 | 1 | |a сверхзвуковые потоки | |
| 610 | 1 | |a экспериментальные исследования | |
| 610 | 1 | |a математическое моделирование | |
| 701 | 1 | |a Maslov |b E. A. |c specialist in the field of power engineering |c Associate Professor of Tomsk Polytechnic University, Candidate of physical and mathematical sciences |f 1982- |g Evgeny Anatolievich |3 (RuTPU)RU\TPU\pers\34319 | |
| 701 | 1 | |a Faraponov |b V. V. | |
| 701 | 1 | |a Arkhipov |b V. A. |g Vladimir Afanasjevich | |
| 701 | 1 | |a Zharova |b I. K. |g Irina Konstantinovna | |
| 701 | 1 | |a Kozlov |b E. A. |g Evgeny Aleksandrovich | |
| 701 | 1 | |a Savkina |b N. V. |g Nadezhda Valerjevna | |
| 712 | 0 | 2 | |a Национальный исследовательский Томский политехнический университет |b Инженерная школа энергетики |b Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова) |3 (RuTPU)RU\TPU\col\23504 |
| 801 | 2 | |a RU |b 63413507 |c 20190627 |g RCR | |
| 856 | 4 | |u https://doi.org/10.2298/TSCI19S2531M | |
| 942 | |c CF | ||