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Wind-tunnel investigation of a spoiler-slot aileron on an NACA 23012 with a full-span Fowler flap
- Author / Creator
- Available as
- Online
- Summary
-
The characteristics of the spoiler-slot aileron of the present investigation are essentially the same as those of the same device on the airfoil with a full-span NACA slotted flap as tested in the ...
The characteristics of the spoiler-slot aileron of the present investigation are essentially the same as those of the same device on the airfoil with a full-span NACA slotted flap as tested in the previous investigation. Up-rigging the ailerons, however, as the flap is deflected may be desirable. The test results indicate that the spoiler-slot aileron will provide acceptable lateral-control characteristics for airplanes with full-span Fowler flaps.
Details
- Creator
- by F.M. Rogallo and Bartholomew S. Spano
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1941
- Physical Details
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- 1 online resource (5, [2] pages) : illustrations
- data file
- OCLC
- on1431128814
- Title from title screen (viewed April 24, 2024)
- Date of issue: December 1941.
- NACA Wartime Report L-376.
- Originally issued as NACA as an Advance Restricted Report.
- Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
- Includes bibliographical references (page 5)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.