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Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects. / Volkov, K. N.; Emel’yanov, V. N.; Karpenko, A. G.; Tolstoguzov, S. S.

In: Journal of Engineering Physics and Thermophysics, Vol. 95, No. 3, 18.06.2022, p. 742-751.

Research output: Contribution to journal › Article › peer-review

Harvard

Volkov, KN, Emel’yanov, VN, Karpenko, AG & Tolstoguzov, SS 2022, 'Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects', Journal of Engineering Physics and Thermophysics, vol. 95, no. 3, pp. 742-751. https://doi.org/10.1007/s10891-022-02532-9

APA

Volkov, K. N., Emel’yanov, V. N., Karpenko, A. G., & Tolstoguzov, S. S. (2022). Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects. Journal of Engineering Physics and Thermophysics, 95(3), 742-751. https://doi.org/10.1007/s10891-022-02532-9

Vancouver

Volkov KN, Emel’yanov VN, Karpenko AG, Tolstoguzov SS. Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects. Journal of Engineering Physics and Thermophysics. 2022 Jun 18;95(3):742-751. https://doi.org/10.1007/s10891-022-02532-9

Author

Volkov, K. N. ; Emel’yanov, V. N. ; Karpenko, A. G. ; Tolstoguzov, S. S. / Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects. In: Journal of Engineering Physics and Thermophysics. 2022 ; Vol. 95, No. 3. pp. 742-751.

BibTeX

@article{2e16911584fc4c2b88b4ef7d3ab9505d,
title = "Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects",
abstract = "The development of a supersonic gas flow over a wedge in the process of interaction of a plane shock wave with the wedge was mathematically simulated on the basis of solution of the Euler equations for the nonstationary flow of a compressible inviscid gas in a two-dimensional space with regard for the high-temperature effects of ionization and dissociation of the gas arising in the gas flow due to the balanced chemical reactions proceeding in it. The results of solution of the problem on the supersonic gas flow over a wedge within the framework of the perfect-gas and real-gas models were compared. The influence of the high-temperature effects in this flow on its characteristics and the angle of inclination of a shock wave in it to the wedge was investigated.",
keywords = "aerodynamics, numerical simulation, physicochemical processes, shock wave, supersonic flow, wedge",
author = "Volkov, {K. N.} and Emel{\textquoteright}yanov, {V. N.} and Karpenko, {A. G.} and Tolstoguzov, {S. S.}",
note = "Volkov, K.N., Emel{\textquoteright}yanov, V.N., Karpenko, A.G. et al. Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects. J Eng Phys Thermophy 95, 742–751 (2022). https://doi.org/10.1007/s10891-022-02532-9",
year = "2022",
month = jun,
day = "18",
doi = "10.1007/s10891-022-02532-9",
language = "English",
volume = "95",
pages = "742--751",
journal = "Journal of Engineering Physics and Thermophysics",
issn = "1062-0125",
publisher = "Springer Nature",
number = "3",

}

RIS

TY - JOUR

T1 - Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects

AU - Volkov, K. N.

AU - Emel’yanov, V. N.

AU - Karpenko, A. G.

AU - Tolstoguzov, S. S.

N1 - Volkov, K.N., Emel’yanov, V.N., Karpenko, A.G. et al. Mathematical Simulation of the Supersonic Gas Flow Over a Wedge with an Attached Shock Wave and High-Temperature Effects. J Eng Phys Thermophy 95, 742–751 (2022). https://doi.org/10.1007/s10891-022-02532-9

PY - 2022/6/18

Y1 - 2022/6/18

N2 - The development of a supersonic gas flow over a wedge in the process of interaction of a plane shock wave with the wedge was mathematically simulated on the basis of solution of the Euler equations for the nonstationary flow of a compressible inviscid gas in a two-dimensional space with regard for the high-temperature effects of ionization and dissociation of the gas arising in the gas flow due to the balanced chemical reactions proceeding in it. The results of solution of the problem on the supersonic gas flow over a wedge within the framework of the perfect-gas and real-gas models were compared. The influence of the high-temperature effects in this flow on its characteristics and the angle of inclination of a shock wave in it to the wedge was investigated.

AB - The development of a supersonic gas flow over a wedge in the process of interaction of a plane shock wave with the wedge was mathematically simulated on the basis of solution of the Euler equations for the nonstationary flow of a compressible inviscid gas in a two-dimensional space with regard for the high-temperature effects of ionization and dissociation of the gas arising in the gas flow due to the balanced chemical reactions proceeding in it. The results of solution of the problem on the supersonic gas flow over a wedge within the framework of the perfect-gas and real-gas models were compared. The influence of the high-temperature effects in this flow on its characteristics and the angle of inclination of a shock wave in it to the wedge was investigated.

KW - aerodynamics

KW - numerical simulation

KW - physicochemical processes

KW - shock wave

KW - supersonic flow

KW - wedge

UR - http://www.scopus.com/inward/record.url?scp=85132365450&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/0d100f25-aaff-388e-a906-1765a0f08feb/

U2 - 10.1007/s10891-022-02532-9

DO - 10.1007/s10891-022-02532-9

M3 - Article

AN - SCOPUS:85132365450

VL - 95

SP - 742

EP - 751

JO - Journal of Engineering Physics and Thermophysics

JF - Journal of Engineering Physics and Thermophysics

SN - 1062-0125

IS - 3

ER -

ID: 97553831