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Computational grid adaptation for the sonic boom near field modeling. / Kiseleva, T.; Temerbekov, V.

In: Journal of Physics: Conference Series, Vol. 1404, No. 1, 012112, 06.12.2019.

Research output: Contribution to journal › Conference article › peer-review

Harvard

Kiseleva, T & Temerbekov, V 2019, 'Computational grid adaptation for the sonic boom near field modeling', Journal of Physics: Conference Series, vol. 1404, no. 1, 012112. https://doi.org/10.1088/1742-6596/1404/1/012112

APA

Kiseleva, T., & Temerbekov, V. (2019). Computational grid adaptation for the sonic boom near field modeling. Journal of Physics: Conference Series, 1404(1), [012112]. https://doi.org/10.1088/1742-6596/1404/1/012112

Vancouver

Kiseleva T, Temerbekov V. Computational grid adaptation for the sonic boom near field modeling. Journal of Physics: Conference Series. 2019 Dec 6;1404(1):012112. doi: 10.1088/1742-6596/1404/1/012112

Author

Kiseleva, T. ; Temerbekov, V. / Computational grid adaptation for the sonic boom near field modeling. In: Journal of Physics: Conference Series. 2019 ; Vol. 1404, No. 1.

BibTeX

@article{118e81d0078143de910fcd4f206b3a2b,
title = "Computational grid adaptation for the sonic boom near field modeling",
abstract = "This paper discusses the numerical simulation of the 69-Degree Delta Wing Body for computing the sonic boom signature in the near field. For flow field calculation, the commercial CFD flow solver ANSYS Fluent is employed. The computational mesh in the perturbed flow regions was refined two times using the automatic gradient adaptation. The results are in agreement with the results obtained by other researchers.",
author = "T. Kiseleva and V. Temerbekov",
year = "2019",
month = dec,
day = "6",
doi = "10.1088/1742-6596/1404/1/012112",
language = "English",
volume = "1404",
journal = "Journal of Physics: Conference Series",
issn = "1742-6588",
publisher = "IOP Publishing Ltd.",
number = "1",
note = "16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 ; Conference date: 30-09-2019 Through 05-10-2019",

}

RIS

TY - JOUR

T1 - Computational grid adaptation for the sonic boom near field modeling

AU - Kiseleva, T.

AU - Temerbekov, V.

PY - 2019/12/6

Y1 - 2019/12/6

N2 - This paper discusses the numerical simulation of the 69-Degree Delta Wing Body for computing the sonic boom signature in the near field. For flow field calculation, the commercial CFD flow solver ANSYS Fluent is employed. The computational mesh in the perturbed flow regions was refined two times using the automatic gradient adaptation. The results are in agreement with the results obtained by other researchers.

AB - This paper discusses the numerical simulation of the 69-Degree Delta Wing Body for computing the sonic boom signature in the near field. For flow field calculation, the commercial CFD flow solver ANSYS Fluent is employed. The computational mesh in the perturbed flow regions was refined two times using the automatic gradient adaptation. The results are in agreement with the results obtained by other researchers.

UR - http://www.scopus.com/inward/record.url?scp=85077816364&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1404/1/012112

DO - 10.1088/1742-6596/1404/1/012112

M3 - Conference article

AN - SCOPUS:85077816364

VL - 1404

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012112

T2 - 16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019

Y2 - 30 September 2019 through 5 October 2019

ER -

ID: 23121335