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NACA-RM-L58C18
Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:05:49Z | |
| date available | 2017-09-04T15:05:49Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | LCYIYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/3288 | |
| description abstract | An investigation has been conducted to determine the effects vertical location of the wing and horizontal tail on the static lateral and directional stability at various combined angles of attack and sideslip for a supersonic airplane configuration at Mach number of 41 and 2.01. The wing had a trapezoidal plan form with an aspect ratio of 3.00, a taper ratio 0.25, and 4-percent-thick circular-arc sections. The horizontal tail was also a trapezoid with an aspect ratio of 4, a taper ratio of 0.6, and NACA 65A006 airfoil sections. | |
| language | English | |
| title | NACA-RM-L58C18 | num |
| title | Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01 | en |
| type | standard | |
| page | 167 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext |
