Reduction of helicopter blade-vortex interaction noise by active rotor control technology /

Reduction of helicopter blade-vortex interaction noise by active rotor control technology /

Bibliographic Details
Corporate Author: United States. National Aeronautics and Space Administration
Other Authors: Yu, Yung H.
Format: Government Document Book
Language:English
Published: [Washington, D.C.] : [National Aeronautics and Space Administration] ; [1997]
Series:NASA technical memorandum ; 207568.
Subjects:
Active control.
Blade-vortex interaction.
Control systems design.
Smart structures.
Structural design.
Helicopters.
AIRCRAFT NOISE.
Harmonic control.

Evans: US Documents Microfiche (3rd floor)

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Call Number: NAS 1.15:207568
 
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NAS 1.15:207568 Available