Standard

Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile. / Zamuraev, V. P.; Kalinina, A. P.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ed. / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. 040021 (AIP Conference Proceedings; Vol. 2027).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Zamuraev, VP & Kalinina, AP 2018, Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile. in Fomin (ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. vol. 2027, 040021, AIP Conference Proceedings, vol. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Russian Federation, 13.08.2018. https://doi.org/10.1063/1.5065295

APA

Zamuraev, V. P., & Kalinina, A. P. (2018). Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile. In Fomin (Ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Vol. 2027). [040021] (AIP Conference Proceedings; Vol. 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065295

Vancouver

Zamuraev VP, Kalinina AP. Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile. In Fomin, editor, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Vol. 2027. American Institute of Physics Inc. 2018. 040021. (AIP Conference Proceedings). doi: 10.1063/1.5065295

Author

Zamuraev, V. P. ; Kalinina, A. P. / Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. editor / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{7a5ab23d5e964be1a1f20e402583778b,
title = "Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile",
abstract = "The effect of two-mode oscillations with frequencies that differ in a twofold is investigated under different energy contributions of each mode. The results of a parametric study of influence of the forced two-mode oscillations of the profile section on the transonic streamline that do not cause either a buffeting or a flutter are obtained. With power decreasing, the increase in lift force is reduced by almost the same factor. Quantitative difference is significant for the lift coefficient at high frequencies for all values of the oscillations power.",
keywords = "VIBRATIONS, AIRFOIL",
author = "Zamuraev, {V. P.} and Kalinina, {A. P.}",
year = "2018",
month = nov,
day = "2",
doi = "10.1063/1.5065295",
language = "English",
volume = "2027",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "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 - Influence of the amplitude-frequency characteristics of two-mode oscillations at unilateral surface effect on the transonic streamline of the symmetrical wing profile

AU - Zamuraev, V. P.

AU - Kalinina, A. P.

PY - 2018/11/2

Y1 - 2018/11/2

N2 - The effect of two-mode oscillations with frequencies that differ in a twofold is investigated under different energy contributions of each mode. The results of a parametric study of influence of the forced two-mode oscillations of the profile section on the transonic streamline that do not cause either a buffeting or a flutter are obtained. With power decreasing, the increase in lift force is reduced by almost the same factor. Quantitative difference is significant for the lift coefficient at high frequencies for all values of the oscillations power.

AB - The effect of two-mode oscillations with frequencies that differ in a twofold is investigated under different energy contributions of each mode. The results of a parametric study of influence of the forced two-mode oscillations of the profile section on the transonic streamline that do not cause either a buffeting or a flutter are obtained. With power decreasing, the increase in lift force is reduced by almost the same factor. Quantitative difference is significant for the lift coefficient at high frequencies for all values of the oscillations power.

KW - VIBRATIONS

KW - AIRFOIL

UR - http://www.scopus.com/inward/record.url?scp=85056320000&partnerID=8YFLogxK

U2 - 10.1063/1.5065295

DO - 10.1063/1.5065295

M3 - Conference contribution

AN - SCOPUS:85056320000

VL - 2027

T3 - AIP Conference Proceedings

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

A2 - Fomin, null

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: 17412096