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Coupled Rotor/Fuselage Dynamic Analysis of the AH-1G Helicopter and Correlation with Flight ... PDF

154 Pages·2015·2.72 MB·English
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Preview Coupled Rotor/Fuselage Dynamic Analysis of the AH-1G Helicopter and Correlation with Flight ...

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A NASTRAN finite element method is used to form isolated fuselage modal characteristics. C81 is then used to couple the rotor and airframe.
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