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Teplofizika vysokikh temperatur, 2018, Volume 56, Issue 2, Pages 270–276
DOI: https://doi.org/10.7868/S0040364418020151
(Mi tvt10739)
 

This article is cited in 6 scientific papers (total in 6 papers)

High Temperature Apparatuses and Structures

Thermodynamic modeling of the composition and characteristics of combustion products of overrich liquid rocket fluids in the quenching mode

A. A. Dorofeev, D. A. Yagodnikov

Bauman Moscow State Technical University
Full-text PDF (259 kB) Citations (6)
References:
Abstract: The working process in the regenerative gas generators of liquid rocket engines is analyzed and a method for computer simulation based on the Zel’dovich’s model of “quenching” the composition of the products of high-temperature combustion as a result of rapid cooling on supplying an excess of the low-temperature component and the resulting chemical quasi-nonequilibrium is developed. The method is implemented and tested on the basis of the TERRA software package in calculations of the composition and properties of the propellant produced by regenerative gas generators using oxygen as the oxidizer and methane as the fuel. The vacuum specific impulse of the considered fuel is calculated for the possible conditions of a quasi-nonequilibrium working process.
Received: 05.09.2016
Accepted: 08.11.2016
English version:
High Temperature, 2018, Volume 56, Issue 2, Pages 263–269
DOI: https://doi.org/10.1134/S0018151X18010066
Bibliographic databases:
Document Type: Article
UDC: 536.46
Language: Russian
Citation: A. A. Dorofeev, D. A. Yagodnikov, “Thermodynamic modeling of the composition and characteristics of combustion products of overrich liquid rocket fluids in the quenching mode”, TVT, 56:2 (2018), 270–276; High Temperature, 56:2 (2018), 263–269
Citation in format AMSBIB
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  • This publication is cited in the following 6 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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