Wind tunnel CESAR model
This document comprises the geometrical definition of a Fowler flap for the LC2B laminar airfoilprovided by DLR. For the purpose of small aircraft, the single slotted Fowler flap for the LC2Blaminar airfoil was designed as a high lift device. This solution ensures a high performance and asimplicity...
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| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-12-01
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| Series: | INCAS Bulletin |
| Online Access: | http://bulletin.incas.ro/files/adrian_dobre_v1no2_full.pdf |
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doaj-94c97b514819479bb66d10c1e66c9263 |
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doaj-94c97b514819479bb66d10c1e66c92632020-11-25T01:13:21ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282009-12-01128589DOI: 10.13111/2066-8201.2009.1.2.13Wind tunnel CESAR modelAdrian DOBREThis document comprises the geometrical definition of a Fowler flap for the LC2B laminar airfoilprovided by DLR. For the purpose of small aircraft, the single slotted Fowler flap for the LC2Blaminar airfoil was designed as a high lift device. This solution ensures a high performance and asimplicity of the design suitable for the intended category of aircrafthttp://bulletin.incas.ro/files/adrian_dobre_v1no2_full.pdf |
| collection |
DOAJ |
| language |
English |
| format |
Article |
| sources |
DOAJ |
| author |
Adrian DOBRE |
| spellingShingle |
Adrian DOBRE Wind tunnel CESAR model INCAS Bulletin |
| author_facet |
Adrian DOBRE |
| author_sort |
Adrian DOBRE |
| title |
Wind tunnel CESAR model |
| title_short |
Wind tunnel CESAR model |
| title_full |
Wind tunnel CESAR model |
| title_fullStr |
Wind tunnel CESAR model |
| title_full_unstemmed |
Wind tunnel CESAR model |
| title_sort |
wind tunnel cesar model |
| publisher |
National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| series |
INCAS Bulletin |
| issn |
2066-8201 2247-4528 |
| publishDate |
2009-12-01 |
| description |
This document comprises the geometrical definition of a Fowler flap for the LC2B laminar airfoilprovided by DLR. For the purpose of small aircraft, the single slotted Fowler flap for the LC2Blaminar airfoil was designed as a high lift device. This solution ensures a high performance and asimplicity of the design suitable for the intended category of aircraft |
| url |
http://bulletin.incas.ro/files/adrian_dobre_v1no2_full.pdf |
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AT adriandobre windtunnelcesarmodel |
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