Standard

The investigation of influence of two-dimensional roughness element on the swept wing flow structure in favourable gradient region. / Kaprilevskaya, V. S.; Kozlov, V. V.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Vasily Fomin. American Institute of Physics Inc., 2018. 040064 (AIP Conference Proceedings; Том 2027).

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

Harvard

Kaprilevskaya, VS & Kozlov, VV 2018, The investigation of influence of two-dimensional roughness element on the swept wing flow structure in favourable gradient region. в V Fomin (ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018., 040064, AIP Conference Proceedings, Том. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Российская Федерация, 13.08.2018. https://doi.org/10.1063/1.5065338

APA

Kaprilevskaya, V. S., & Kozlov, V. V. (2018). The investigation of influence of two-dimensional roughness element on the swept wing flow structure in favourable gradient region. в V. Fomin (Ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 [040064] (AIP Conference Proceedings; Том 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065338

Vancouver

Kaprilevskaya VS, Kozlov VV. The investigation of influence of two-dimensional roughness element on the swept wing flow structure in favourable gradient region. в Fomin V, Редактор, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. American Institute of Physics Inc. 2018. 040064. (AIP Conference Proceedings). doi: 10.1063/1.5065338

Author

Kaprilevskaya, V. S. ; Kozlov, V. V. / The investigation of influence of two-dimensional roughness element on the swept wing flow structure in favourable gradient region. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Редактор / Vasily Fomin. American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{9bfbca58c8c14988a4d783ea3fccfa49,
title = "The investigation of influence of two-dimensional roughness element on the swept wing flow structure in favourable gradient region",
abstract = "The paper given considers the investigation results of stationary and secondary disturbances development behind two-dimensional roughness element. When lying upstream the three-dimensional roughness element induced the disturbances which were affected by two-dimensional roughness lying further downstream. In this case the two-dimensional roughness caused the appearance of stationary structures. Also there were secondary perturbations with frequency range different from the case of excitement by three-dimensional roughness.",
keywords = "BOUNDARY-LAYER",
author = "Kaprilevskaya, {V. S.} and Kozlov, {V. V.}",
year = "2018",
month = nov,
day = "2",
doi = "10.1063/1.5065338",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Vasily Fomin",
booktitle = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018",
note = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 ; Conference date: 13-08-2018 Through 19-08-2018",

}

RIS

TY - GEN

T1 - The investigation of influence of two-dimensional roughness element on the swept wing flow structure in favourable gradient region

AU - Kaprilevskaya, V. S.

AU - Kozlov, V. V.

PY - 2018/11/2

Y1 - 2018/11/2

N2 - The paper given considers the investigation results of stationary and secondary disturbances development behind two-dimensional roughness element. When lying upstream the three-dimensional roughness element induced the disturbances which were affected by two-dimensional roughness lying further downstream. In this case the two-dimensional roughness caused the appearance of stationary structures. Also there were secondary perturbations with frequency range different from the case of excitement by three-dimensional roughness.

AB - The paper given considers the investigation results of stationary and secondary disturbances development behind two-dimensional roughness element. When lying upstream the three-dimensional roughness element induced the disturbances which were affected by two-dimensional roughness lying further downstream. In this case the two-dimensional roughness caused the appearance of stationary structures. Also there were secondary perturbations with frequency range different from the case of excitement by three-dimensional roughness.

KW - BOUNDARY-LAYER

UR - http://www.scopus.com/inward/record.url?scp=85056300451&partnerID=8YFLogxK

U2 - 10.1063/1.5065338

DO - 10.1063/1.5065338

M3 - Conference contribution

AN - SCOPUS:85056300451

T3 - AIP Conference Proceedings

BT - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

A2 - Fomin, Vasily

PB - American Institute of Physics Inc.

T2 - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

Y2 - 13 August 2018 through 19 August 2018

ER -

ID: 25833569