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Performance data from a wind-tunnel test of two main-rotor blade designs for a utility-class helicopter /

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Main Author: Singleton, Jeffrey D.
Corporate Authors: United States. Army Aviation Research and Technology Activity, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors: Yeager, William T., Wilbur, Matthew L.
Format: Government Document Microfilm Book
Language:English
Published: [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990.
Series:NASA technical memorandum ; 4183.
AVSCOM technical memorandum ; 90-B-004.
Subjects:
Rotors (Helicopters) > Aerodynamics > Statistics.
Aeroelasticity.
Helicopters.
Wind tunnels.
Rotors (Helicopters) > Aerodynamics.
Rotors (Helicopters)
Statistics.
Online Access: Online Access
Item Description:Shipping list no.: 90-0857-M.
Physical Description:79 pages : illustrations ; 28 cm.
Also available via Internet from the NASA Technical Report Server web site. Address as of 8/16/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011658%5F1990011658.pdf ; current access is available via PURL.
Reproduction Note:Microfiche.

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