http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed
1 online resource (iv, 43 pages) : color illustrations.
"Performing organization: NASA Langley Research Center"--Report documentation page.
Includes bibliographical references (pages 16-17).
Sponsored by the National Aeronautics and Space Administration 147016.03.07.04.02