Trim Analysis of Tandem Helicopter
Aeronautical Computing Technique(2008)
摘要
Two mathematical models for determining the trims of a tandem helicopter using two techniques are built separately in this paper,one among which is based on the momentum theory and the other is based on the rotor vortex theory.And the comparison of trim analysis figures has shown a good agreement with the referenced test results,and the models are the basis of analysis for determining derivatives.
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关键词
helicopter,tandem
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