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

Bibliographic Details
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 Microform Book
Language:	English
Published:	[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1990.
Series:	AVSCOM technical memorandum ; 90-B-004. NASA technical memorandum ; 4183.
Subjects:	Rotors (Helicopters) > Aerodynamics > Statistics. Aeroelasticity. Dynamic structural analysis. Helicopter performance. Performance tests. Rotary wings. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/LPS62831

Description
Item Description:	Microform.
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.
Bibliography:	Includes bibliographical references (pages 4-5).