RESEARCH OF INFLUENCE OF PERFORATION TO REDUCE PULSATION LOADS ACTING ON THE AERODYNAMIC CONTROL SURFACES

RESEARCH OF INFLUENCE OF PERFORATION TO REDUCE PULSATION LOADS ACTING ON THE AERODYNAMIC CONTROL SURFACES

The research of unsteady vortex flow influence on the aerodynamic control and stabilizing surfaces is carried out. There are defined pulsation aerodynamic characteristics of flight controls with using the open software OpenFoam. The results of the numerical calculations of flow around brake flap and...

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Bibliographic Details
Main Authors: V. T. Kalugin, A. S. Epikhin, P. A. Chernukha
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
Subjects:
открытый пакет openfoam
модель турбулентности les
нестационарные вихревые течения
бафтинговые нагрузки
тормозной щиток
перфорация
килевой стабилизатор
Online Access:https://avia.mstuca.ru/jour/article/view/251

Internet

https://avia.mstuca.ru/jour/article/view/251

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