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NACA-TN-1417
High-speed wind-tunnel tests of an NACA 0009-64 airfoil having a 33.4-percent-chord flap with an overhang 20.1 percent of the flap chord
Year: 1947
Abstract: INTRODUCTION
Flight and wind-tunnel studies have show that compressibility will have serious adverse effects on the characteristics of the usual flap type control surface. In order to investigate these effects two flapped airfoils were tested in the Langley 24-inch high-speed tunnel. Tests of the first airfoil, and NACA 16-009, were reported in reference 1. The results of the tests of the second airfoil, an NACA 0009-64, are given herein.
Flight and wind-tunnel studies have show that compressibility will have serious adverse effects on the characteristics of the usual flap type control surface. In order to investigate these effects two flapped airfoils were tested in the Langley 24-inch high-speed tunnel. Tests of the first airfoil, and NACA 16-009, were reported in reference 1. The results of the tests of the second airfoil, an NACA 0009-64, are given herein.
Subject: AIRFOILS
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:13:38Z | |
| date available | 2017-09-04T15:13:38Z | |
| date copyright | 01/01/1947 | |
| date issued | 1947 | |
| identifier other | MATSYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/12308 | |
| description abstract | INTRODUCTION Flight and wind-tunnel studies have show that compressibility will have serious adverse effects on the characteristics of the usual flap type control surface. In order to investigate these effects two flapped airfoils were tested in the Langley 24-inch high-speed tunnel. Tests of the first airfoil, and NACA 16-009, were reported in reference 1. The results of the tests of the second airfoil, an NACA 0009-64, are given herein. | |
| language | English | |
| title | NACA-TN-1417 | num |
| title | High-speed wind-tunnel tests of an NACA 0009-64 airfoil having a 33.4-percent-chord flap with an overhang 20.1 percent of the flap chord | en |
| type | standard | |
| page | 34 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext | |
| subject keywords | AIRFOILS | |
| subject keywords | CHAR | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | COMPRESSIBILITY | |
| subject keywords | EFFECT | |
| subject keywords | FLAPS | |
| subject keywords | HIGH | |
| subject keywords | MOMENTS | |
| subject keywords | NACA | |
| subject keywords | OVERHANG | |
| subject keywords | SPEED | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND | |
| subject keywords | WING |