Tunnel-wall corrections to rolling and yawing moments due to aileron deflection in closed rectangular wind tunnels / by Donald J. Graham.
A method is developed for calculating the tunnel-wall corrections to rolling and yawing moments due to aileron deflection on models in closed rectangular wind tunnels. Graphs are presented which permit a rapid determination of these corrections for models mounted in 7- by 10-foot or 8- by 12-foot wi...
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| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series A. |
| 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. A14. |
| Subjects: |
MARC
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| 100 | 1 | |a Graham, Donald J. | |
| 245 | 1 | 0 | |a Tunnel-wall corrections to rolling and yawing moments due to aileron deflection in closed rectangular wind tunnels / |c by Donald J. Graham. |
| 246 | 3 | |a NACA Wartime Reports. Series A. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1945] | ||
| 300 | |a 28 pages, 5 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. A14. | |
| 500 | |a NACA Wartime Report A-14. | ||
| 500 | |a Originally issued as NACA Advance Restricted Report 4F21(January 1945) | ||
| 500 | |a Prepared at the Ames Aeronautical Laboratory, Moffett Field, California. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A method is developed for calculating the tunnel-wall corrections to rolling and yawing moments due to aileron deflection on models in closed rectangular wind tunnels. Graphs are presented which permit a rapid determination of these corrections for models mounted in 7- by 10-foot or 8- by 12-foot wind tunnels. The method is so developed that the corrections may be calculated for the deflection of either aileron alone or both ailerons simultaneously. | |
| 650 | 0 | |a Ailerons. |0 http://id.loc.gov/authorities/subjects/sh85002551. | |
| 650 | 0 | |a Rolling (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85114890. | |
| 650 | 0 | |a Yawing (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85149046. | |
| 650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292. | |
| 650 | 0 | |a Mathematics. |0 http://id.loc.gov/authorities/subjects/sh85082139. | |
| 650 | 7 | |a Ailerons. |2 fast |0 (OCoLC)fst00802020. | |
| 650 | 7 | |a Mathematics. |2 fast |0 (OCoLC)fst01012163. | |
| 650 | 7 | |a Rolling (Aerodynamics) |2 fast |0 (OCoLC)fst01099689. | |
| 650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047. | |
| 650 | 7 | |a Yawing (Aerodynamics) |2 fast |0 (OCoLC)fst01182552. | |
| 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 Ames Research Center. |0 http://id.loc.gov/authorities/names/n79138699 |1 http://isni.org/isni/0000000119557990. | |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. A14. | |
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