To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber
- 作者: Pelevin F.V.1, Ponomarev A.V.1
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隶属关系:
- Bauman Moscow State Technical University (National Research University)
- 期: 卷 61, 编号 1 (2018)
- 页面: 71-77
- 栏目: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230409
- DOI: https://doi.org/10.3103/S1068799818010117
- ID: 230409
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详细
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.
作者简介
F. Pelevin
Bauman Moscow State Technical University (National Research University)
编辑信件的主要联系方式.
Email: pelfv@rambler.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
A. Ponomarev
Bauman Moscow State Technical University (National Research University)
Email: pelfv@rambler.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
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