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

Evans: US Documents Microfiche (3rd floor)