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俄罗斯空气动力研究所中心学报

ISSN 打印: 1948-2590
ISSN 在线: 1948-2604

俄罗斯空气动力研究所中心学报

DOI: 10.1615/TsAGISciJ.2017020745
pages 11-24

NUMERICAL INVESTIGATIONS OF THE EFFECTS OF SHAPES AND SIZES OF THE GAP BETWEEN THE LIFTING SURFACE AND CONTROL SURFACE WITH THE OVERHANG BALANCE ON ITS EFFECTIVENESS AND HINGE MOMENT

Vladimir Valeryevich Bogatyrev
Central Aerohydrodynamic Institute, 1, Zhukovsky Str., Zhukovsky, Moscow Region, 140180 Russia

ABSTRACT

Numerical investigations were carried out of the two- and three-dimensional flow around a lifting surface with a symmetrical cross section and a deflected control surface with an overhang balance. The influence of several versions of the gap between the lifting and control surfaces on the aerodynamic characteristics was studied. Increased effectiveness and reduced hinge moment of the control surface were achieved by the proper choice of the gap parameters and shape.


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