Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method /

Bibliographic Details

Main Author:	Riley, Donald R. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015.
Series:	NASA technical memorandum ; 2015-218998.
Subjects:	Aerodynamic coefficients. Aerodynamic stability. Airfoils. Time dependence. Vortices.
Online Access:	https://purl.fdlp.gov/GPO/gpo67295 http://purl.fdlp.gov/GPO/gpo67295