VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT

The results of computational and experimental study of thin wings flutter in separated and unseparated flow are presented. The effect of flutter suppressing in the presence of separation is found.

Bibliographic Details
Main Authors: V. V. Ovchinnikov, Yu. V. Petrov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/652
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spelling doaj-acb8dfbc880744d4ba4473b9b1733c332021-07-28T21:00:37ZrusMoscow State Technical University of Civil Aviation Naučnyj Vestnik MGTU GA2079-06192542-01192016-11-012175762652VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENTV. V. Ovchinnikov0Yu. V. Petrov1Академия ГПС МЧС РоссииМГТУ ГАThe results of computational and experimental study of thin wings flutter in separated and unseparated flow are presented. The effect of flutter suppressing in the presence of separation is found.https://avia.mstuca.ru/jour/article/view/652аэроупругостьфлаттерколебанияотрывное обтеканиерасчетно-экспериментальная методика
collection DOAJ
language Russian
format Article
sources DOAJ
author V. V. Ovchinnikov
Yu. V. Petrov
spellingShingle V. V. Ovchinnikov
Yu. V. Petrov
VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
Naučnyj Vestnik MGTU GA
аэроупругость
флаттер
колебания
отрывное обтекание
расчетно-экспериментальная методика
author_facet V. V. Ovchinnikov
Yu. V. Petrov
author_sort V. V. Ovchinnikov
title VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
title_short VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
title_full VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
title_fullStr VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
title_full_unstemmed VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
title_sort vibrations of thin wings in the separated flow. calculation and experiment
publisher Moscow State Technical University of Civil Aviation
series Naučnyj Vestnik MGTU GA
issn 2079-0619
2542-0119
publishDate 2016-11-01
description The results of computational and experimental study of thin wings flutter in separated and unseparated flow are presented. The effect of flutter suppressing in the presence of separation is found.
topic аэроупругость
флаттер
колебания
отрывное обтекание
расчетно-экспериментальная методика
url https://avia.mstuca.ru/jour/article/view/652
work_keys_str_mv AT vvovchinnikov vibrationsofthinwingsintheseparatedflowcalculationandexperiment
AT yuvpetrov vibrationsofthinwingsintheseparatedflowcalculationandexperiment
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