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Крутильно-изгибный флаттер крыла : математические модели, исследование и предотвращение. Обзор. / Andrievsky, B.; Kuznetsov, N. V.; Kudryashova, E. V.; Kuznetsova, O. A.

In: Differencialnie Uravnenia i Protsesy Upravlenia, Vol. 2021, No. 4, 2021, p. 116-191.

Research output: Contribution to journal › Article › peer-review

Harvard

Andrievsky, B, Kuznetsov, NV, Kudryashova, EV & Kuznetsova, OA 2021, 'Крутильно-изгибный флаттер крыла: математические модели, исследование и предотвращение. Обзор', Differencialnie Uravnenia i Protsesy Upravlenia, vol. 2021, no. 4, pp. 116-191.

APA

Andrievsky, B., Kuznetsov, N. V., Kudryashova, E. V., & Kuznetsova, O. A. (2021). Крутильно-изгибный флаттер крыла: математические модели, исследование и предотвращение. Обзор. Differencialnie Uravnenia i Protsesy Upravlenia, 2021(4), 116-191.

Vancouver

Andrievsky B, Kuznetsov NV, Kudryashova EV, Kuznetsova OA. Крутильно-изгибный флаттер крыла: математические модели, исследование и предотвращение. Обзор. Differencialnie Uravnenia i Protsesy Upravlenia. 2021;2021(4):116-191.

Author

Andrievsky, B. ; Kuznetsov, N. V. ; Kudryashova, E. V. ; Kuznetsova, O. A. / Крутильно-изгибный флаттер крыла : математические модели, исследование и предотвращение. Обзор. In: Differencialnie Uravnenia i Protsesy Upravlenia. 2021 ; Vol. 2021, No. 4. pp. 116-191.

BibTeX

@article{df6a39622b294cfe9c81752f08e537f1,
title = "Крутильно-изгибный флаттер крыла: математические модели, исследование и предотвращение. Обзор",
abstract = "Depending on the flight mode, the airflow can either damp aircraft oscillations, or, conversely, the oscillating structure takes energy from the incoming flow, as a result of which a rapid increase in amplitude of oscillations may occur. This dangerous phenomenon has become a significant obstacle to the development of high-speed aviation. Since the 1930s and up to the present time, the efforts of many researchers are aimed at describing the dynamics of this phenomenon, studying its properties and developing measures to prevent it. In the present paper, some existing results on elastic-flexural wing flutter are surveyed. The paper starts from various ways of modeling the elastic-flexural wing flutter. The results on investigations of the elastic-flexural wing flutter phenomenon are reviewed, and several approaches of passive and active flutter suppression methods are described.",
keywords = "analysis, hidden oscillations, modeling, suppression, wing flutter",
author = "B. Andrievsky and Kuznetsov, {N. V.} and Kudryashova, {E. V.} and Kuznetsova, {O. A.}",
note = "Funding Information: This work was supported by a grant from Leading Scientific schools of the Russian Federation for 2020–2021, project NSh-2624.2020.1 (chapters 1, 2) and St. Petersburg State University, project Pure ID 75207094 (chapters 3–5). Funding Information: В статье [165] представлены результаты, полученные с помощью моде-ли работы [166] в ходе испытаний, проведенных в калибровочной (CWT) и низкоскоростной (LSWT) аэродинамической трубах в Совете по науч-ным и промышленным исследованиям (Council for Scientific and Industrial Research, CSIR).3 Publisher Copyright: {\textcopyright} 2021 Saint-Petersburg State University. All rights reserved.",
year = "2021",
language = "русский",
volume = "2021",
pages = "116--191",
journal = "ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ",
issn = "1817-2172",
publisher = "Электронный журнал {"}Дифференциальные уравнения и процессы управления{"}",
number = "4",

}

RIS

TY - JOUR

T1 - Крутильно-изгибный флаттер крыла

T2 - математические модели, исследование и предотвращение. Обзор

AU - Andrievsky, B.

AU - Kuznetsov, N. V.

AU - Kudryashova, E. V.

AU - Kuznetsova, O. A.

N1 - Funding Information: This work was supported by a grant from Leading Scientific schools of the Russian Federation for 2020–2021, project NSh-2624.2020.1 (chapters 1, 2) and St. Petersburg State University, project Pure ID 75207094 (chapters 3–5). Funding Information: В статье [165] представлены результаты, полученные с помощью моде-ли работы [166] в ходе испытаний, проведенных в калибровочной (CWT) и низкоскоростной (LSWT) аэродинамической трубах в Совете по науч-ным и промышленным исследованиям (Council for Scientific and Industrial Research, CSIR).3 Publisher Copyright: © 2021 Saint-Petersburg State University. All rights reserved.

PY - 2021

Y1 - 2021

N2 - Depending on the flight mode, the airflow can either damp aircraft oscillations, or, conversely, the oscillating structure takes energy from the incoming flow, as a result of which a rapid increase in amplitude of oscillations may occur. This dangerous phenomenon has become a significant obstacle to the development of high-speed aviation. Since the 1930s and up to the present time, the efforts of many researchers are aimed at describing the dynamics of this phenomenon, studying its properties and developing measures to prevent it. In the present paper, some existing results on elastic-flexural wing flutter are surveyed. The paper starts from various ways of modeling the elastic-flexural wing flutter. The results on investigations of the elastic-flexural wing flutter phenomenon are reviewed, and several approaches of passive and active flutter suppression methods are described.

AB - Depending on the flight mode, the airflow can either damp aircraft oscillations, or, conversely, the oscillating structure takes energy from the incoming flow, as a result of which a rapid increase in amplitude of oscillations may occur. This dangerous phenomenon has become a significant obstacle to the development of high-speed aviation. Since the 1930s and up to the present time, the efforts of many researchers are aimed at describing the dynamics of this phenomenon, studying its properties and developing measures to prevent it. In the present paper, some existing results on elastic-flexural wing flutter are surveyed. The paper starts from various ways of modeling the elastic-flexural wing flutter. The results on investigations of the elastic-flexural wing flutter phenomenon are reviewed, and several approaches of passive and active flutter suppression methods are described.

KW - analysis

KW - hidden oscillations

KW - modeling

KW - suppression

KW - wing flutter

UR - http://www.scopus.com/inward/record.url?scp=85129646285&partnerID=8YFLogxK

M3 - статья

AN - SCOPUS:85129646285

VL - 2021

SP - 116

EP - 191

JO - ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ

JF - ДИФФЕРЕНЦИАЛЬНЫЕ УРАВНЕНИЯ И ПРОЦЕССЫ УПРАВЛЕНИЯ

SN - 1817-2172

IS - 4

ER -

ID: 95231248