A study of the effects of vertical tail area and dihedral on the lateral maneuverability of an airplane / by Leo F. Fehlner.
A theoretical investigation has been made of the influence of changes in vertical tail area and dihedral angle on the lateral flying characteristics of an airplane. The lateral motions were computed for nine different combinations of vertical tail area and dihedral, covering the range of parameters...
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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,
[1941]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L347. |
| Subjects: |
MARC
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| 100 | 1 | |a Fehlner, Leo F. |0 http://id.loc.gov/authorities/names/no2006104550 |1 http://isni.org/isni/0000000048258685. | |
| 245 | 1 | 2 | |a A study of the effects of vertical tail area and dihedral on the lateral maneuverability of an airplane / |c by Leo F. Fehlner. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1941] | ||
| 300 | |a 20 pages, 3 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. L347. | |
| 500 | |a NACA Wartime Report L-347. | ||
| 500 | |a Originally issued as NACA as an Advance Restricted Report (October 1941) | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A theoretical investigation has been made of the influence of changes in vertical tail area and dihedral angle on the lateral flying characteristics of an airplane. The lateral motions were computed for nine different combinations of vertical tail area and dihedral, covering the range of parameters used in the design of typical airplanes. The motions were initiated by aileron and rudder controls, and consideration was given to various amounts of yawing moment accompanying aileron control. | |
| 650 | 0 | |a Ailerons. |0 http://id.loc.gov/authorities/subjects/sh85002551. | |
| 650 | 0 | |a Airplanes |x Handling characteristics. |0 http://id.loc.gov/authorities/subjects/sh85002825. | |
| 650 | 0 | |a Airplanes |x Control. | |
| 650 | 0 | |a Airplanes |x Tail surfaces. |0 http://id.loc.gov/authorities/subjects/sh85002903. | |
| 650 | 0 | |a Airplanes |x Dihedral wings. |0 http://id.loc.gov/authorities/subjects/sh2002010118. | |
| 650 | 0 | |a Stability of airplanes, Lateral. |0 http://id.loc.gov/authorities/subjects/sh85127187. | |
| 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. |2 fast |0 (OCoLC)fst00803107. | |
| 650 | 7 | |a Airplanes |x Dihedral wings. |2 fast |0 (OCoLC)fst00803147. | |
| 650 | 7 | |a Airplanes |x Handling characteristics. |2 fast |0 (OCoLC)fst00803228. | |
| 650 | 7 | |a Airplanes |x Tail surfaces. |2 fast |0 (OCoLC)fst00803481. | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast |0 (OCoLC)fst00852545. | |
| 650 | 7 | |a Stability of airplanes, Lateral. |2 fast |0 (OCoLC)fst01131215. | |
| 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. L347. | |
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