Standard

Calculation of transonic flow past the twisted wings. / Ryabinin, Anatoly.

2015 International Conference on Mechanics - Seventh Polyakhov's Reading. ред. / A. A. Tikhonov. Institute of Electrical and Electronics Engineers Inc., 2015. 7106768 (2015 International Conference on Mechanics - Seventh Polyakhov's Reading).

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › Рецензирование

Harvard

Ryabinin, A 2015, Calculation of transonic flow past the twisted wings. в AA Tikhonov (ред.), 2015 International Conference on Mechanics - Seventh Polyakhov's Reading., 7106768, 2015 International Conference on Mechanics - Seventh Polyakhov's Reading, Institute of Electrical and Electronics Engineers Inc., VII Поляховские чтения, Saint Petersburg, Российская Федерация, 2/02/15. https://doi.org/10.1109/POLYAKHOV.2015.7106768, https://doi.org/10.1109/POLYAKHOV.2015.7106768

APA

Ryabinin, A. (2015). Calculation of transonic flow past the twisted wings. в A. A. Tikhonov (Ред.), 2015 International Conference on Mechanics - Seventh Polyakhov's Reading [7106768] (2015 International Conference on Mechanics - Seventh Polyakhov's Reading). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/POLYAKHOV.2015.7106768, https://doi.org/10.1109/POLYAKHOV.2015.7106768

Vancouver

Ryabinin A. Calculation of transonic flow past the twisted wings. в Tikhonov AA, Редактор, 2015 International Conference on Mechanics - Seventh Polyakhov's Reading. Institute of Electrical and Electronics Engineers Inc. 2015. 7106768. (2015 International Conference on Mechanics - Seventh Polyakhov's Reading). https://doi.org/10.1109/POLYAKHOV.2015.7106768, https://doi.org/10.1109/POLYAKHOV.2015.7106768

Author

Ryabinin, Anatoly. / Calculation of transonic flow past the twisted wings. 2015 International Conference on Mechanics - Seventh Polyakhov's Reading. Редактор / A. A. Tikhonov. Institute of Electrical and Electronics Engineers Inc., 2015. (2015 International Conference on Mechanics - Seventh Polyakhov's Reading).

BibTeX

@inproceedings{d581a40718bd4c67bfb20d22e486e337,
title = "Calculation of transonic flow past the twisted wings",
abstract = "The spatial flow around an asymmetric wing segment J-78 with a twist is studied. Solutions of Reynolds-averaged Navier-Stokes equations are obtained with Ansys CFX - 13 finite volume solver. A three-dimensional mesh with elongated along the wing span elements near the wing is used. The pressure distribution on the wing surface is studied in the certain range of average angle of attack. This range corresponds to coalescence and splitting of the super-sonic regions above the upper surface of the wing.",
author = "Anatoly Ryabinin",
note = "Publisher Copyright: {\textcopyright} 2015 IEEE. Copyright: Copyright 2015 Elsevier B.V., All rights reserved.; 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOV'S READING : SEVENTH POLYAKHOV'S READING ; Conference date: 02-02-2015 Through 06-02-2015",
year = "2015",
month = may,
day = "13",
doi = "10.1109/POLYAKHOV.2015.7106768",
language = "English",
series = "2015 International Conference on Mechanics - Seventh Polyakhov's Reading",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
editor = "Tikhonov, {A. A.}",
booktitle = "2015 International Conference on Mechanics - Seventh Polyakhov's Reading",
address = "United States",
url = "http://pol2015.math.spbu.ru/en/, http://pol2015.math.spbu.ru/en/about/, http://pol2015.math.spbu.ru/",

}

RIS

TY - GEN

T1 - Calculation of transonic flow past the twisted wings

AU - Ryabinin, Anatoly

N1 - Conference code: 7

PY - 2015/5/13

Y1 - 2015/5/13

N2 - The spatial flow around an asymmetric wing segment J-78 with a twist is studied. Solutions of Reynolds-averaged Navier-Stokes equations are obtained with Ansys CFX - 13 finite volume solver. A three-dimensional mesh with elongated along the wing span elements near the wing is used. The pressure distribution on the wing surface is studied in the certain range of average angle of attack. This range corresponds to coalescence and splitting of the super-sonic regions above the upper surface of the wing.

AB - The spatial flow around an asymmetric wing segment J-78 with a twist is studied. Solutions of Reynolds-averaged Navier-Stokes equations are obtained with Ansys CFX - 13 finite volume solver. A three-dimensional mesh with elongated along the wing span elements near the wing is used. The pressure distribution on the wing surface is studied in the certain range of average angle of attack. This range corresponds to coalescence and splitting of the super-sonic regions above the upper surface of the wing.

UR - http://www.scopus.com/inward/record.url?scp=84938250183&partnerID=8YFLogxK

U2 - 10.1109/POLYAKHOV.2015.7106768

DO - 10.1109/POLYAKHOV.2015.7106768

M3 - Conference contribution

T3 - 2015 International Conference on Mechanics - Seventh Polyakhov's Reading

BT - 2015 International Conference on Mechanics - Seventh Polyakhov's Reading

A2 - Tikhonov, A. A.

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOV'S READING

Y2 - 2 February 2015 through 6 February 2015

ER -

ID: 3932616