Numerical simulation of sonic boom near-field flow over 69-degree delta wing body

Standard

Numerical simulation of sonic boom near-field flow over 69-degree delta wing body. / Kiseleva, T.; Lukeshevich, S.

In: Journal of Physics: Conference Series, Vol. 1404, No. 1, 012111, 06.12.2019.

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

Harvard

Kiseleva, T & Lukeshevich, S 2019, 'Numerical simulation of sonic boom near-field flow over 69-degree delta wing body', Journal of Physics: Conference Series, vol. 1404, no. 1, 012111. https://doi.org/10.1088/1742-6596/1404/1/012111

APA

Kiseleva, T., & Lukeshevich, S. (2019). Numerical simulation of sonic boom near-field flow over 69-degree delta wing body. Journal of Physics: Conference Series, 1404(1), [012111]. https://doi.org/10.1088/1742-6596/1404/1/012111

Vancouver

Kiseleva T, Lukeshevich S. Numerical simulation of sonic boom near-field flow over 69-degree delta wing body. Journal of Physics: Conference Series. 2019 Dec 6;1404(1):012111. doi: 10.1088/1742-6596/1404/1/012111

Author

Kiseleva, T. ; Lukeshevich, S. / Numerical simulation of sonic boom near-field flow over 69-degree delta wing body. In: Journal of Physics: Conference Series. 2019 ; Vol. 1404, No. 1.

BibTeX

@article{a2ddb99bfd994fadb739b2e4e0baf029,

title = "Numerical simulation of sonic boom near-field flow over 69-degree delta wing body",

abstract = "Fast and accurate prediction of sonic boom intensity is important in performing design and optimization studies of a supersonic aircraft. The paper presents the computational mesh generation technique for sonic boom prediction in the near field of complex geometry body. Studies are done on a 69-degree delta wing body model used for testing various prediction techniques in the framework of the AIAA Sonic Boom Prediction Workshops.",

author = "T. Kiseleva and S. Lukeshevich",

note = "Publisher Copyright: {\textcopyright} 2019 IOP Publishing Ltd. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 ; Conference date: 30-09-2019 Through 05-10-2019",

year = "2019",

month = dec,

day = "6",

doi = "10.1088/1742-6596/1404/1/012111",

language = "English",

volume = "1404",

journal = "Journal of Physics: Conference Series",

issn = "1742-6588",

publisher = "IOP Publishing Ltd.",

number = "1",

}

RIS

TY - JOUR

T1 - Numerical simulation of sonic boom near-field flow over 69-degree delta wing body

AU - Kiseleva, T.

AU - Lukeshevich, S.

PY - 2019/12/6

Y1 - 2019/12/6

N2 - Fast and accurate prediction of sonic boom intensity is important in performing design and optimization studies of a supersonic aircraft. The paper presents the computational mesh generation technique for sonic boom prediction in the near field of complex geometry body. Studies are done on a 69-degree delta wing body model used for testing various prediction techniques in the framework of the AIAA Sonic Boom Prediction Workshops.

AB - Fast and accurate prediction of sonic boom intensity is important in performing design and optimization studies of a supersonic aircraft. The paper presents the computational mesh generation technique for sonic boom prediction in the near field of complex geometry body. Studies are done on a 69-degree delta wing body model used for testing various prediction techniques in the framework of the AIAA Sonic Boom Prediction Workshops.

UR - http://www.scopus.com/inward/record.url?scp=85077814945&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1404/1/012111

DO - 10.1088/1742-6596/1404/1/012111

M3 - Conference article

AN - SCOPUS:85077814945

VL - 1404

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012111

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: 23121386