Computational aspects of helicopter trim analysis and damping levels from Floquet theory

An edition of Computational aspects of helicopter trim analysis and damping levels from Floquet theory (1992)

Computational aspects of helicopter trim analysis and damping levels from Floquet theory

final technical report under NASA-Ames Research grant no. NAG 2-727 (August 1, 1991 - July 31, 1992)

By G. H. Gaonkar

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Publish Date

1992

Publisher

Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering,National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Helicopters, Damping, Vibration (Aeronautics), Handling characteristics