درباره ما
NACA-RM-L55D08
Exploratory investigation at Mach number 4.06 of an airplane configuration having a wing of trapezoidal plan form effects of various tail arrangements on wing-on and wing-off static longitudinal and lateral stability characteristics
Year: 1955
Abstract: INTRODUCTION
The airplane configurations previously investigated experimentally at high supersonic and hypersonic speeds have been restricted to misssile types which were not required to land and which, therefore, had relatively small wings or wings of very low aspect ratio. The purpose of the present investigation is to determine the characteristics of a configuration conforming more closely to a piloted airplane having a wing area sufficient for conventional landing.
In references 2, 3, and 4 longitudinal and lateral stability data were presented, and in references 5 and 6 longitudinal and lateral control data were presented for this airplane configuration and various combinations of its components at Mach numbers of 4 .06 and 6.86. This report presents, at a Mach number of 4.06, the effects of various combinations of the horizontal and vertical tails on the airplane with and without the wing. The data have been analyzed only to the extent that some stability determinants have been obtained.
The airplane configurations previously investigated experimentally at high supersonic and hypersonic speeds have been restricted to misssile types which were not required to land and which, therefore, had relatively small wings or wings of very low aspect ratio. The purpose of the present investigation is to determine the characteristics of a configuration conforming more closely to a piloted airplane having a wing area sufficient for conventional landing.
In references 2, 3, and 4 longitudinal and lateral stability data were presented, and in references 5 and 6 longitudinal and lateral control data were presented for this airplane configuration and various combinations of its components at Mach numbers of 4 .06 and 6.86. This report presents, at a Mach number of 4.06, the effects of various combinations of the horizontal and vertical tails on the airplane with and without the wing. The data have been analyzed only to the extent that some stability determinants have been obtained.
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:18:06Z | |
| date available | 2017-09-04T18:18:06Z | |
| date copyright | 01/01/1955 | |
| date issued | 1955 | |
| identifier other | HQSWXDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/200865 | |
| description abstract | INTRODUCTION The airplane configurations previously investigated experimentally at high supersonic and hypersonic speeds have been restricted to misssile types which were not required to land and which, therefore, had relatively small wings or wings of very low aspect ratio. The purpose of the present investigation is to determine the characteristics of a configuration conforming more closely to a piloted airplane having a wing area sufficient for conventional landing. In references 2, 3, and 4 longitudinal and lateral stability data were presented, and in references 5 and 6 longitudinal and lateral control data were presented for this airplane configuration and various combinations of its components at Mach numbers of 4 .06 and 6.86. This report presents, at a Mach number of 4.06, the effects of various combinations of the horizontal and vertical tails on the airplane with and without the wing. The data have been analyzed only to the extent that some stability determinants have been obtained. | |
| language | English | |
| title | NACA-RM-L55D08 | num |
| title | Exploratory investigation at Mach number 4.06 of an airplane configuration having a wing of trapezoidal plan form effects of various tail arrangements on wing-on and wing-off static longitudinal and lateral stability characteristics | en |
| type | standard | |
| page | 61 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1955 | |
| contenttype | fulltext |