Calculation of stick forces for an elevator with a spring tab / by Harry Greenberg.
Formulas for the calculation of hinge-moment characteristics of an elevator with a spring tab have been developed in terms of aerodynamic parameters, spring stiffness, and airspeed. The formulas have been used in a study of the stick-force gradients on a pursuit airplane equipped with an elevator wi...
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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,
[1944]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L129. |
| Subjects: |
MARC
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| 100 | 1 | |a Greenberg, Harry. |0 http://id.loc.gov/authorities/names/no2006094222. | |
| 245 | 1 | 0 | |a Calculation of stick forces for an elevator with a spring tab / |c by Harry Greenberg. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1944] | ||
| 300 | |a 15 pages, 6 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. L129. | |
| 500 | |a NACA Wartime Report L-129. | ||
| 500 | |a Originally issued as NACA as Restricted Bulletin L4F07 (June 1944) | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Formulas for the calculation of hinge-moment characteristics of an elevator with a spring tab have been developed in terms of aerodynamic parameters, spring stiffness, and airspeed. The formulas have been used in a study of the stick-force gradients on a pursuit airplane equipped with an elevator with a spring tab. Charts are presented showing the variation of stick-force gradient in accelerated flight over a large range of speed and the complete range of spring stiffness for various center-of-gravity locations, altitudes, and airplane sizes. | |
| 650 | 0 | |a Airplanes |x Control. | |
| 650 | 0 | |a Elevators (Airplanes) |0 http://id.loc.gov/authorities/subjects/sh85042561. | |
| 650 | 0 | |a Hinge moments (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85060958. | |
| 650 | 0 | |a Tabs (Airplanes) |0 http://id.loc.gov/authorities/subjects/sh85131827. | |
| 650 | 0 | |a Mathematics. |0 http://id.loc.gov/authorities/subjects/sh85082139. | |
| 650 | 0 | |a Charts, diagrams, etc. |0 http://id.loc.gov/authorities/subjects/sh87002373. | |
| 650 | 7 | |a Airplanes |x Control. |2 fast |0 (OCoLC)fst00803107. | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast |0 (OCoLC)fst00852545. | |
| 650 | 7 | |a Elevators (Airplanes) |2 fast |0 (OCoLC)fst00908089. | |
| 650 | 7 | |a Hinge moments (Aerodynamics) |2 fast |0 (OCoLC)fst00957213. | |
| 650 | 7 | |a Mathematics. |2 fast |0 (OCoLC)fst01012163. | |
| 650 | 7 | |a Tabs (Airplanes) |2 fast |0 (OCoLC)fst01141800. | |
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| 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. L129. | |
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