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The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover /

Bibliographic Details
Main Author: Bousman, William G.
Corporate Authors: Ames Research Center, United States. Army Aviation Research and Technology Activity
Format: Government Document Microform Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1990.
Series:AVSCOM technical report ; 89-A-002.
NASA technical paper ; 3002.
Subjects:
Rotors (Helicopters) > Stability.
Rotors (Helicopters) > Aerodynamics.
Aeroelasticity.
Coupling.
Hovering.
Hovering stability.
Mathematical models.
Rigid rotors.
Rotary wings.
Online Access:https://purl.fdlp.gov/GPO/LPS65436

Internet

https://purl.fdlp.gov/GPO/LPS65436

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Call Number: NAS 1.60:3002
 
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Holdings details from Available Online
Call Number: NAS 1.60:3002
 
Call Number Status Get It
NAS 1.60:3002 Available