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Reduction of blade-vortex interaction noise using higher harmonic pitch control /

Bibliographic Details
Corporate Authors: Langley Research Center, United States. Army Aviation Research and Technology Activity
Other Authors: Brooks, Thomas F.
Format: Government Document Book
Language:English
Published: Hampton, Va. : US Army Aviation Systems Command, Aviation R & T Activity, National Aeronautics and Space Administration, Langley Research Center ; [1989]
Series:NASA technical memorandum ; 101624.
AVSCOM technical memorandum ; 89-B-005.
Subjects:
Rotors > Noise.
Acoustics.
Blade-vortex interaction.
Control systems design.
Noise reduction.
Pitch (Inclination)
Propeller noise.
Online Access:https://purl.fdlp.gov/GPO/LPS108702

Internet

https://purl.fdlp.gov/GPO/LPS108702

Available Online

Holdings details from Available Online
Call Number: NAS 1.15:101624
 
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NAS 1.15:101624 Available