Abstract The results of stress analysis for the main rotor torsion bar of the ANSAT helicopter based on the finite element method are presented. The analysis was performed for the base types of loading in the linear statement. The analysis results agree well with the experimental data.
Stress analysis of helicopter main rotor torsion bar
Russian Aeronautics (Iz VUZ) ; 52 , 1 ; 104-109
2009-03-01
6 pages
Article (Journal)
Electronic Resource
English
Stress analysis of helicopter main rotor torsion bar
Online Contents | 2009
|Helicopter main-rotor/tail-rotor interaction
Tema Archive | 2000
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