Abstract
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 thermoprobe. 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.
| Original language | English |
|---|---|
| Pages (from-to) | S531-S536 |
| Journal | Thermal Science |
| Volume | 23 |
| DOIs | |
| Publication status | Published - 1 Jan 2019 |
Fingerprint
Keywords
- Experimental research
- Gas dynamics
- Heat transfer
- Mathematical modeling
- Supersonic flow
ASJC Scopus subject areas
- Renewable Energy, Sustainability and the Environment
Cite this
Investigation of working processes in a flowing channel of ramjet engine. / Maslov, Eugene; Faraponov, Valery; Arkhipov, Vladimir; Zharova, Irina; Kozlov, Eugene; Savkina, Nadezhda.
In: Thermal Science, Vol. 23, 01.01.2019, p. S531-S536.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Investigation of working processes in a flowing channel of ramjet engine
AU - Maslov, Eugene
AU - Faraponov, Valery
AU - Arkhipov, Vladimir
AU - Zharova, Irina
AU - Kozlov, Eugene
AU - Savkina, Nadezhda
PY - 2019/1/1
Y1 - 2019/1/1
N2 - 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 thermoprobe. 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.
AB - 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 thermoprobe. 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.
KW - Experimental research
KW - Gas dynamics
KW - Heat transfer
KW - Mathematical modeling
KW - Supersonic flow
UR - http://www.scopus.com/inward/record.url?scp=85065208700&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85065208700&partnerID=8YFLogxK
U2 - 10.2298/TSCI19S2531M
DO - 10.2298/TSCI19S2531M
M3 - Article
AN - SCOPUS:85065208700
VL - 23
SP - S531-S536
JO - Thermal Science
JF - Thermal Science
SN - 0354-9836
ER -