VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
Abstract
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.
About the Authors
V. V. Ovchinnikov
Академия ГПС МЧС России
Russian Federation
Russian Federation
Yu. V. Petrov
МГТУ ГА
Russian Federation
Russian Federation
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Review
For citations:
Ovchinnikov V.V., Petrov Yu.V. VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT. Civil Aviation High Technologies. 2015;(217):57-62. (In Russ.)
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