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

Record details

  • Physical Description: 1 online resource (61 pages) : illustrations.
  • Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 2015.

Content descriptions

General Note: Title from title screen (viewed April 26, 2016).
"December 2015."
"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
L-20616

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