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

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