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NACA-WR-L-710
Determination of the stability and control characteristics of airplanes from tests of powered models
Year: 1942
Abstract: A technique of testing wind-tunnel powered models has been developed as a result of experience gained in the investigation of the static longitudinal and lateral-stability and control characteristics of several powered models in the NACA 7- by 10-foot wind tunnel. As an important part of this technique, a minimum program of the tests considered necessary to specify satisfactorily the static stability and control characteristics for present-day airplanes has been tentatively established.
A discussion of the conditions to be investigated, methods of presenting and interpreting the data, and a suggested operating technique are given. Typical test data, illustrating some of the effects of power on the characteristics of a model of a low-wing single-engine airplane, are also presented.
A discussion of the conditions to be investigated, methods of presenting and interpreting the data, and a suggested operating technique are given. Typical test data, illustrating some of the effects of power on the characteristics of a model of a low-wing single-engine airplane, are also presented.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:54:39Z | |
| date available | 2017-09-04T15:54:39Z | |
| date copyright | 01/01/1942 | |
| date issued | 1942 | |
| identifier other | QTCZYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/58074 | |
| description abstract | A technique of testing wind-tunnel powered models has been developed as a result of experience gained in the investigation of the static longitudinal and lateral-stability and control characteristics of several powered models in the NACA 7- by 10-foot wind tunnel. As an important part of this technique, a minimum program of the tests considered necessary to specify satisfactorily the static stability and control characteristics for present-day airplanes has been tentatively established. A discussion of the conditions to be investigated, methods of presenting and interpreting the data, and a suggested operating technique are given. Typical test data, illustrating some of the effects of power on the characteristics of a model of a low-wing single-engine airplane, are also presented. | |
| language | English | |
| title | NACA-WR-L-710 | num |
| title | Determination of the stability and control characteristics of airplanes from tests of powered models | en |
| type | standard | |
| page | 79 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1942 | |
| contenttype | fulltext |