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NACA-TN-3797
Section characteristics of the NACA 0006 airfoil with leading-edge and trailing-edge flaps
Year: 1956
Abstract: Lift and pitching-moment characteristics of an NACA 0006 airfoil are presented for various deflections of a 0.15-chord leading-edge flap and a 0.30-chord plain trailing-edge flap. Pressure-distribution data are presented in tabular form. The data were obtained at a Mach number of 0.15 and a Reynolds number of 4,500,000.
Subject: EDGE
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:31:20Z | |
| date available | 2017-09-04T18:31:20Z | |
| date copyright | 01/01/1956 | |
| date issued | 1956 | |
| identifier other | IYNUYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/213549 | |
| description abstract | Lift and pitching-moment characteristics of an NACA 0006 airfoil are presented for various deflections of a 0.15-chord leading-edge flap and a 0.30-chord plain trailing-edge flap. Pressure-distribution data are presented in tabular form. The data were obtained at a Mach number of 0.15 and a Reynolds number of 4,500,000. | |
| language | English | |
| title | NACA-TN-3797 | num |
| title | Section characteristics of the NACA 0006 airfoil with leading-edge and trailing-edge flaps | en |
| type | standard | |
| page | 18 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1956 | |
| contenttype | fulltext | |
| subject keywords | EDGE | |
| subject keywords | FLAPS | |
| subject keywords | LEADING | |
| subject keywords | LOADS | |
| subject keywords | PLAIN | |
| subject keywords | SECTIONS | |
| subject keywords | STEADY | |
| subject keywords | WING | |
| subject keywords | WINGS |