Hinge moments of sealed-internal-balance arrangements for control surfaces. : 2 - Experimental investigation of fabric seals in the presence of a thin-plate overhang / by Jack Fischel.
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, a...
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| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L52. |
| Subjects: |
MARC
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| 100 | 1 | |a Fischel, Jack. |0 http://id.loc.gov/authorities/names/n88613237. | |
| 245 | 1 | 0 | |a Hinge moments of sealed-internal-balance arrangements for control surfaces. : |b 2 - Experimental investigation of fabric seals in the presence of a thin-plate overhang / |c by Jack Fischel. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1945] | ||
| 300 | |a 16 pages, 36 unnumbered pages : |b illustrations ; |c 27 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 490 | 1 | |a Wartime Report / National Advisory Committee for Aeronautics ; |v no. L52. | |
| 500 | |a NACA Wartime Report L-52. | ||
| 500 | |a Originally issued as NACA as Advance Restricted Report L5F30a (August 1945) | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a 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. | |
| 650 | 0 | |a Airplanes |x Control surfaces. |0 http://id.loc.gov/authorities/subjects/sh85002798. | |
| 650 | 0 | |a Ailerons. |0 http://id.loc.gov/authorities/subjects/sh85002551. | |
| 650 | 0 | |a Hinge moments (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85060958. | |
| 650 | 0 | |a Flaps (Airplanes) |0 http://id.loc.gov/authorities/subjects/sh85049001. | |
| 650 | 0 | |a Charts, diagrams, etc. |0 http://id.loc.gov/authorities/subjects/sh87002373. | |
| 650 | 7 | |a Ailerons. |2 fast |0 (OCoLC)fst00802020. | |
| 650 | 7 | |a Airplanes |x Control surfaces. |2 fast |0 (OCoLC)fst00803108. | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast |0 (OCoLC)fst00852545. | |
| 650 | 7 | |a Flaps (Airplanes) |2 fast |0 (OCoLC)fst00927038. | |
| 650 | 7 | |a Hinge moments (Aerodynamics) |2 fast |0 (OCoLC)fst00957213. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://isni.org/isni/0000000106642010. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. |0 http://id.loc.gov/authorities/names/n81018841. | |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L52. | |
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