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NASA-CR-2214
Two-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems. Volume 1: Data analysis
Year: 1977
Abstract: High-lift systems for a NASA, 9.3%, method for calculating the viscous flow about two-dimensional multicomponent airfoils was evaluated by comparing its predictions with test data. High-lift systems derived from supercritical airfoils were compared in terms of performance to high-lift systems derived from conventional airfoils. The high-lift systems for the supercritical airfoil were designed to achieve maximum lift and consisted of: a single-slotted flap; a double-slotted flap and a leading-edge slat; and a triple-slotted flap and a leading-edge slat. Agreement between theoretical predictions and experimental results are also discussed.
Subject: AIRFOILS
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:32:21Z | |
| date available | 2017-09-04T15:32:21Z | |
| date copyright | 01/01/1977 | |
| date issued | 1977 | |
| identifier other | OGNKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/33979 | |
| description abstract | High-lift systems for a NASA, 9.3%, method for calculating the viscous flow about two-dimensional multicomponent airfoils was evaluated by comparing its predictions with test data. High-lift systems derived from supercritical airfoils were compared in terms of performance to high-lift systems derived from conventional airfoils. The high-lift systems for the supercritical airfoil were designed to achieve maximum lift and consisted of: a single-slotted flap; a double-slotted flap and a leading-edge slat; and a triple-slotted flap and a leading-edge slat. Agreement between theoretical predictions and experimental results are also discussed. | |
| language | English | |
| title | NASA-CR-2214 | num |
| title | Two-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems. Volume 1: Data analysis | en |
| type | standard | |
| page | 91 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1977 | |
| contenttype | fulltext | |
| subject keywords | AIRFOILS | |
| subject keywords | BOUNDARY | |
| subject keywords | CONTROL | |
| subject keywords | DIMENSIONAL | |
| subject keywords | EDGE | |
| subject keywords | LAYER | |
| subject keywords | LEADING | |
| subject keywords | LIFT | |
| subject keywords | SLATS | |
| subject keywords | SUPERCRITICAL | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | TWO | |
| subject keywords | WAKES | |
| subject keywords | WIND | |
| subject keywords | WINGS |