To Calculation of Regenerative Cooling of a Liquid Fuel Rocket Engine Chamber


Citar

Texto integral

Acesso aberto Acesso aberto
Acesso é fechado Acesso está concedido
Acesso é fechado Somente assinantes

Resumo

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.

Sobre autores

F. Pelevin

Bauman Moscow State Technical University (National Research University)

Autor responsável pela correspondência
Email: pelfv@rambler.ru
Rússia, ul. 2-ya Baumanskaya 5, Moscow, 105005

A. Ponomarev

Bauman Moscow State Technical University (National Research University)

Email: pelfv@rambler.ru
Rússia, ul. 2-ya Baumanskaya 5, Moscow, 105005

Arquivos suplementares

Arquivos suplementares
Ação
1. JATS XML

Declaração de direitos autorais © Allerton Press, Inc., 2018