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Title Free wake analysis of hover performance using a new influence coefficent method [electronic resource] / Todd R. Quackenbush ... [et al.].

Imprint

[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.

Connect to
Connect to http://purl.access.gpo.gov/GPO/LPS67089

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.26:4309	---	Available

Description	vii, 93 p. : ill. ; 28 cm.
Series	NASA contractor report ; 4309
	NASA contractor report ; NASA CR-4309.
Note	Prepared at Continuum Dynamics, Inc., for Ames Research Center under Contract NAS2-12148.
	"July 1990."
Form	Mode of access via the NTRS web site.
Bibliography	Bibliography: p. 77-79.
Subject	Rotors (Helicopters) -- Aerodynamics -- Computer simulation.
	Wakes (Aerodynamics) -- Computer simulation.
	Computer programs.
	Free flow.
	Helicopter performance.
	Helicopter wakes.
	Hovering stability.
	Influence coeffcient.
Added Author	Quackenbush, Todd R.
	Continuum Dynamics, Inc.
	Ames Research Center.
	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Gpo Item No.	0830-H-14 (online)
Sudoc No.	NAS 1.26:4309