Free wake analysis of hover performance using a new influence coefficent method /

Bibliographic Details
Corporate Authors:	Continuum Dynamics, Inc, Ames Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Quackenbush, Todd R.
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:	NASA contractor report ; NASA CR-4309.
Subjects:	Rotors (Helicopters) > Aerodynamics > Computer simulation. Wakes (Aerodynamics) > Computer simulation. Computer programs. Free flow. Helicopter performance. Helicopter wakes. Hovering stability. Influence coeffcient.
Online Access:	https://purl.fdlp.gov/GPO/LPS67089

Description
Item Description:	Shipping list number: 1991-0818-M. Prepared at Continuum Dynamics, Inc., for Ames Research Center under Contract NAS2-12148. "July 1990." Microform.
Physical Description:	vii, 93 pages : illustrations ; 28 cm. Also available via Internet from the NTRS web site. Address as of 2/16/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910009737%5F1991009737.pdf; current access is available via PURL.
Bibliography:	Bibliography: pages 77-79.