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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.


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

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