Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets /

Bibliographic Details
Main Author:	Kelley, Henry L.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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 memorandum ; 90-B-015. NASA technical memorandum ; 4201.
Subjects:	Helicopters > Aerodynamics. Rotors (Helicopters) > Aerodynamics. Apache (Attack helicopter) Aerodynamic characteristics. AH-64 helicopter. Ground effect (Aerodynamics) Helicopter performance. Rotor aerodynamics. Wind tunnel models. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/LPS61086

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