Investigation of working processes in a flowing channel of ramjet engine

The technique and results of experimental-theoretical study of gas-dynamics, heat transfer and the structure of gas-flow in the flowing channel of a ramjet engine in Mach number range M = (5-7) are presented. The temperature distribution along the flowing channel of a ramjet engine was expe...

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Main Authors:	Maslov Eugene, Faraponov Valery, Arkhipov Vladimir, Zharova Irina, Kozlov Eugene, Savkina Nadezhda
Format:	Article
Language:	English
Published:	VINCA Institute of Nuclear Sciences 2019-01-01
Series:	Thermal Science
Subjects:	gas dynamics heat transfer supersonic flow experimental research mathematical modeling
Online Access:	http://www.doiserbia.nb.rs/img/doi/0354-9836/2019/0354-983619531M .pdf

id	doaj-8e8ae1dd1ace4494bd28ea1e99104a23
record_format	Article
spelling	doaj-8e8ae1dd1ace4494bd28ea1e99104a232021-01-02T11:05:39ZengVINCA Institute of Nuclear SciencesThermal Science0354-98362019-01-0123Suppl. 253153610.2298/TSCI19S2531M0354-983619531MInvestigation of working processes in a flowing channel of ramjet engineMaslov Eugene0Faraponov Valery1Arkhipov Vladimir2Zharova Irina3Kozlov Eugene4Savkina Nadezhda5National Research Tomsk State University, Tomsk, Russia + National Research Tomsk Polytechnic University, Tomsk, RussiaNational Research Tomsk State University, Tomsk, RussiaNational Research Tomsk State University, Tomsk, RussiaNational Research Tomsk State University, Tomsk, RussiaNational Research Tomsk State University, Tomsk, RussiaNational Research Tomsk State University, Tomsk, RussiaThe technique and results of experimental-theoretical study of gas-dynamics, heat transfer and the structure of gas-flow in the flowing channel of a ramjet engine in Mach number range M = (5-7) are presented. The temperature distribution along the flowing channel of a ramjet engine was experimentally obtained. The temperature along the wall of the flowing channel of the axisymmetric model was measured using the developed thermo-probe. Distributions of Mach number and temperature along the symmetry axis of the flowing channel of the model are obtained numerically. Comparison of the numerical and experimentally obtained values of the Mach number showed their qualitative agreement.http://www.doiserbia.nb.rs/img/doi/0354-9836/2019/0354-983619531M .pdfgas dynamicsheat transfersupersonic flowexperimental researchmathematical modeling
collection	DOAJ
language	English
format	Article
sources	DOAJ
author	Maslov Eugene Faraponov Valery Arkhipov Vladimir Zharova Irina Kozlov Eugene Savkina Nadezhda
spellingShingle	Maslov Eugene Faraponov Valery Arkhipov Vladimir Zharova Irina Kozlov Eugene Savkina Nadezhda Investigation of working processes in a flowing channel of ramjet engine Thermal Science gas dynamics heat transfer supersonic flow experimental research mathematical modeling
author_facet	Maslov Eugene Faraponov Valery Arkhipov Vladimir Zharova Irina Kozlov Eugene Savkina Nadezhda
author_sort	Maslov Eugene
title	Investigation of working processes in a flowing channel of ramjet engine
title_short	Investigation of working processes in a flowing channel of ramjet engine
title_full	Investigation of working processes in a flowing channel of ramjet engine
title_fullStr	Investigation of working processes in a flowing channel of ramjet engine
title_full_unstemmed	Investigation of working processes in a flowing channel of ramjet engine
title_sort	investigation of working processes in a flowing channel of ramjet engine
publisher	VINCA Institute of Nuclear Sciences
series	Thermal Science
issn	0354-9836
publishDate	2019-01-01
description	The technique and results of experimental-theoretical study of gas-dynamics, heat transfer and the structure of gas-flow in the flowing channel of a ramjet engine in Mach number range M = (5-7) are presented. The temperature distribution along the flowing channel of a ramjet engine was experimentally obtained. The temperature along the wall of the flowing channel of the axisymmetric model was measured using the developed thermo-probe. Distributions of Mach number and temperature along the symmetry axis of the flowing channel of the model are obtained numerically. Comparison of the numerical and experimentally obtained values of the Mach number showed their qualitative agreement.
topic	gas dynamics heat transfer supersonic flow experimental research mathematical modeling
url	http://www.doiserbia.nb.rs/img/doi/0354-9836/2019/0354-983619531M .pdf
work_keys_str_mv	AT masloveugene investigationofworkingprocessesinaflowingchanneloframjetengine AT faraponovvalery investigationofworkingprocessesinaflowingchanneloframjetengine AT arkhipovvladimir investigationofworkingprocessesinaflowingchanneloframjetengine AT zharovairina investigationofworkingprocessesinaflowingchanneloframjetengine AT kozloveugene investigationofworkingprocessesinaflowingchanneloframjetengine AT savkinanadezhda investigationofworkingprocessesinaflowingchanneloframjetengine
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Investigation of working processes in a flowing channel of ramjet engine

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