Investigation at zero forward speed of a leading-edge slat as a longitudinal control device for vertically rising airplanes that utilize the redirected-slipstream principle Page: 1 of 34
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zNATIONAL ADVISORY COMMITTEE
FOR AERONAUTICSTECHNICAL NOTE 3692
INVESTIGATION AT ZERO FORWARD SPEED OF A LEADING-EDGE
SLAT AS A LONGITUDINAL CONTROL DEVICE FOR
VERTICALLY RISING AIRPLANES THAT UTILIZE
THE REDIRECTED-SLIPSTREAM PRINCIPLE
By Richard E. Kutmbn
Langley Aeronautical Laboratory
Langley Field, Va.
NACA
Washington
May 1956m -m
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Kuhn, Richard E. Investigation at zero forward speed of a leading-edge slat as a longitudinal control device for vertically rising airplanes that utilize the redirected-slipstream principle, report, May 1956; (https://digital.library.unt.edu/ark:/67531/metadc55950/m1/1/: accessed April 23, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.