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Hinge moments of sealed-internal-balance arrangements for control surfaces. 2 - Experimental investigation of fabric seals in the presence of a thin-plate overhang
- Author / Creator
- Available as
- Online
- Summary
-
Tests were made in a seal test chamber to determine the hinge moments contributed by the fabric seal in an internal-balance arrangement employing a thin-plate over-hang. These tests were performed ...
Tests were made in a seal test chamber to determine the hinge moments contributed by the fabric seal in an internal-balance arrangement employing a thin-plate over-hang. These tests were performed with various widths of fabric sealing various widths of flap-nose gap, with a horizontal, a vertical, and a circular type wing structure forward of the balance, and with various heights of balance chamber.
Details
- Creator
- by Jack Fischel
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1945
- Physical Details
-
- 1 online resource (16, [36] pages) : illustrations
- data file
- OCLC
- on1302882254
- NACA Wartime Report L-52.
- Originally issued as NACA as Advance Restricted Report L5F30a (August 1945).
- Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
- Includes bibliographical references.
Subjects
- Airplanes -- Control surfaces.
- Ailerons.
- Hinge moments (Aerodynamics)
- Flaps (Airplanes)
- Charts, diagrams, etc.
- diagrams.
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