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Coupled rotor/fuselage vibration analysis using detailed 3-D airframe models.

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Publication:5952775
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DOI10.1016/S0895-7177(00)00299-5zbMath1197.74056OpenAlexW2103969788MaRDI QIDQ5952775

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Publication date: 22 January 2002

Published in: Mathematical and Computer Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0895-7177(00)00299-5


zbMATH Keywords

AH-1G helicopterhelicopter vibrationNASTRAN airframerotor/fuselage coupling


Mathematics Subject Classification ID

Application models in control theory (93C95) Vibrations in dynamical problems in solid mechanics (74H45)


Related Items (1)

Rotorcraft fuselage/main rotor coupling dynamics modelling and analysis







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