Методика расчета течений рабочих тел в газодинамических трактах ПВРД
| Parent link: | Перспективы развития фундаментальных наук=Prospects of Fundamental Sciences Development: сборник научных трудов XIV Международной конференции студентов, аспирантов и молодых ученых, г. Томск, 25-28 апреля 2017 г./ Национальный исследовательский Томский политехнический университет (ТПУ) ; под ред. И. А. Курзиной, Г. А. Вороновой.— , 2017 Т. 1 : Физика.— 2017.— [С. 174-176] |
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| Glavni autor: | |
| Daljnji autori: | , , |
| Sažetak: | Заглавие с экрана In the present study calculations algorithm of gas flow of ramjet engine are shown. The algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for ramjet model which consists of air intake, combustion chamber, nozzle and supersonic jet. The results in agreement with known solutions for cold blowing of ramjet gas-dynamic paths. |
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2017
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| Teme: | |
| Online pristup: | http://earchive.tpu.ru/handle/11683/44158 |
| Format: | Elektronički Poglavlje knjige |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=624373 |
| Sažetak: | Заглавие с экрана In the present study calculations algorithm of gas flow of ramjet engine are shown. The algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for ramjet model which consists of air intake, combustion chamber, nozzle and supersonic jet. The results in agreement with known solutions for cold blowing of ramjet gas-dynamic paths. |
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