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

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.

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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:	Научный вестник МГТУ ГА
Subjects:	aeroelasticity flutter vibrations separated flow computational and experimental method
Online Access:	https://avia.mstuca.ru/jour/article/view/652
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