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NACA-TN-1291
Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates
Year: 1947
Abstract: INTRODUCTION
In order to provide fundamental design data the National Advisory Committee for Aeronautics has undertaken the expedient of publishing collections of data obtained in specific investigations and, whenever possible, analysis of the data. The present paper contains a Collection and analysis of data that includes 19 tail surfaces tested in the Langley 4- by 6-foot vertical tunnel. These tail surfaces are from complete airplane models that have been tested for stability and control characteristics the Langley 7- by 10-foot tunnel. Some data from other tunnels (references 1 to 5) are presented for comparisons. In addition, some data are presented on tests of isolated tails cut to various spans and equipped with end plates of various shapes.
In order to provide fundamental design data the National Advisory Committee for Aeronautics has undertaken the expedient of publishing collections of data obtained in specific investigations and, whenever possible, analysis of the data. The present paper contains a Collection and analysis of data that includes 19 tail surfaces tested in the Langley 4- by 6-foot vertical tunnel. These tail surfaces are from complete airplane models that have been tested for stability and control characteristics the Langley 7- by 10-foot tunnel. Some data from other tunnels (references 1 to 5) are presented for comparisons. In addition, some data are presented on tests of isolated tails cut to various spans and equipped with end plates of various shapes.
Subject: AIRFOILS
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:37:22Z | |
| date available | 2017-09-04T17:37:22Z | |
| date copyright | 01/01/1947 | |
| date issued | 1947 | |
| identifier other | DMYIYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/160258 | |
| description abstract | INTRODUCTION In order to provide fundamental design data the National Advisory Committee for Aeronautics has undertaken the expedient of publishing collections of data obtained in specific investigations and, whenever possible, analysis of the data. The present paper contains a Collection and analysis of data that includes 19 tail surfaces tested in the Langley 4- by 6-foot vertical tunnel. These tail surfaces are from complete airplane models that have been tested for stability and control characteristics the Langley 7- by 10-foot tunnel. Some data from other tunnels (references 1 to 5) are presented for comparisons. In addition, some data are presented on tests of isolated tails cut to various spans and equipped with end plates of various shapes. | |
| language | English | |
| title | NACA-TN-1291 | num |
| title | Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates | en |
| type | standard | |
| page | 170 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext | |
| subject keywords | AIRFOILS | |
| subject keywords | CHAR | |
| subject keywords | CLARK | |
| subject keywords | ELEVATORS | |
| subject keywords | END | |
| subject keywords | HINGE | |
| subject keywords | HORIZONTAL | |
| subject keywords | LIFT | |
| subject keywords | LIFTING | |
| subject keywords | MOMENTS | |
| subject keywords | NACA | |
| subject keywords | ORDINATES | |
| subject keywords | ORDINATS | |
| subject keywords | PLATES | |
| subject keywords | SURFACE | |
| subject keywords | SURFACES | |
| subject keywords | TAIL | |
| subject keywords | THEORIES |