Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method / Donald R. Riley.
- Physical Description: 1 online resource (61 pages) : illustrations.
- Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015.
|General Note:|| Title from title screen (viewed April 26, 2016).
"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
|Bibliography, etc. Note:|| Includes bibliographical references (page 14).
|Funding Information Note:|| Sponsored by the National Aeronautics and Space Administration 432938.11.01.07.43.40.17
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