Coupled rotor/fuselage vibration analysis using detailed 3-D airframe models-Reference-Cited by-同舟云学术

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

Published:2001-05 Issue:10-11 Volume:33 Page:1035-1054
ISSN:0895-7177
Container-title:Mathematical and Computer Modelling
language:en
Short-container-title:Mathematical and Computer Modelling

Author:

Yeo Hyeonsoo,Chopra I.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modelling and Simulation

Reference18 articles.

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4. Validation of rotor vibratory airloads and application to helicopter response;Yen;Journal of the American Helicopter Society,1990

5. Challenge of predicting helicopter vibration;Miao;Proceedings of the AHS International Meeting on Advanced Rotorcraft Technology and Disaster Relief,1998

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