To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber
- Авторлар: Pelevin F.V.1, Ponomarev A.V.1
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Мекемелер:
- Bauman Moscow State Technical University (National Research University)
- Шығарылым: Том 61, № 1 (2018)
- Беттер: 71-77
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230409
- DOI: https://doi.org/10.3103/S1068799818010117
- ID: 230409
Дәйексөз келтіру
Аннотация
This paper demonstrates that in transition from the one-dimensional longitudinal-channel motion of the coolant in the regenerative cooling system of the liquid propellant engine to the twodimensional (interchannel) channel motion (transpiration) through a porous mesh material (PMM), the hydraulic losses decrease. Experimental data on PMM hydraulic resistance coefficients and heat transfer in porous paths with the interchannel coolant transpiration (ICCT) is presented.
Авторлар туралы
F. Pelevin
Bauman Moscow State Technical University (National Research University)
Хат алмасуға жауапты Автор.
Email: pelfv@rambler.ru
Ресей, ul. 2-ya Baumanskaya 5, Moscow, 105005
A. Ponomarev
Bauman Moscow State Technical University (National Research University)
Email: pelfv@rambler.ru
Ресей, ul. 2-ya Baumanskaya 5, Moscow, 105005
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