Publication Date:
2013-08-31
Description:
The results of an analytical study aimed at predicting the aeromechanical stability of a helicopter in ground resonance, with the inclusion of aerodynamic forces are presented. The theoretical results are found to be in good agreement with the experimental results, available in literature, indicating that the coupled rotor/fuselage system can be represented by a reasonably simple mathematical model.
Keywords:
AIRCRAFT STABILITY AND CONTROL
Type:
NASA, Ames Research Center, Integrated Technology Rotor Methodology Assessment Workshop; p 253-26
Format:
application/pdf
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