Cover Image

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
Description
Item Description:Title from title screen (viewed April 26, 2016).
"December 2015."
"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
Physical Description:1 online resource (61 pages) : illustrations.
Bibliography:Includes bibliographical references (page 14).