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Validation of a model for a two-bladed flexible rotor system - Progress to date
1999
37th Aerospace Sciences Meeting and Exhibit
unpublished
NOTICE This report was prepared as an account of work sponsored by an agency of the United States government. Neither the United States government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific
doi:10.2514/6.1999-60
fatcat:cmiknvz66zbt3dg3rmv4bftiza