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NACA-TR-627
The experimental and calculated characteristics of 22 tapered wings
Year: 1938
Abstract: The experimental and calculated aerodynamic characteristics of 22 tapered wings are compared, using tests made in the variable-density wind tunnel. The wings had aspect ratios from 6 to 12 and taper ratios from 1:6:1 and 5:1. The compared characteristics are the pitching moment, the aerodynamic-center position, the lift-curve slope, the maximum lift coefficient, and the curves of drag. The method of obtaining the calculated values is based on the use of wing theory and experimentally determined airfoil section data. In general, the experimental and calculated characteristics are in sufficiently good agreement that the method may be applied to many problems of airplane design.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:19:37Z | |
| date available | 2017-09-04T15:19:37Z | |
| date copyright | 01/01/1938 | |
| date issued | 1938 | |
| identifier other | MTWUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/19467 | |
| description abstract | The experimental and calculated aerodynamic characteristics of 22 tapered wings are compared, using tests made in the variable-density wind tunnel. The wings had aspect ratios from 6 to 12 and taper ratios from 1:6:1 and 5:1. The compared characteristics are the pitching moment, the aerodynamic-center position, the lift-curve slope, the maximum lift coefficient, and the curves of drag. The method of obtaining the calculated values is based on the use of wing theory and experimentally determined airfoil section data. In general, the experimental and calculated characteristics are in sufficiently good agreement that the method may be applied to many problems of airplane design. | |
| language | English | |
| title | NACA-TR-627 | num |
| title | The experimental and calculated characteristics of 22 tapered wings | en |
| type | standard | |
| page | 30 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1938 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | BALANCE | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | CHORDS | |
| subject keywords | COEFFICIENTS | |
| subject keywords | COMPARISON | |
| subject keywords | COMPUTATIONAL | |
| subject keywords | DRAG | |
| subject keywords | DYNAMICS | |
| subject keywords | EFFECT | |
| subject keywords | FLUID | |
| subject keywords | GEOMETRY | |
| subject keywords | LIFT | |
| subject keywords | MOMENTS | |
| subject keywords | PITCHING | |
| subject keywords | PROFILES | |
| subject keywords | RATIO | |
| subject keywords | SCALE | |
| subject keywords | SWEPT | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND | |
| subject keywords | WING | |
| subject keywords | WINGS |