The Analysis of Hinge Moment Round Height Rudders Rotate Axis of the Gliders Lak-17b, Changing Aerodynamic Compensation Area
Olegas Kalitončikas
Abstract
In the article glider's LAK-17B hinge moment around the spin axis during the stabilized flight, when changing the aerodynamic compensation area and flap angles was analyzed. Calculations were performed in Microsoft Excel and Autodesk Inventor Professional 2011 programs. The results are presented graphically.
Article in Lithuanian
Article in:
Lithuanian
Article published:
2013-01-23
Keyword(s): flap; loading; strength; hinge moment; aerodynamic compensation
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