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NASA-TN-D-4076
Static stability characteristics at Mach numbers from 1.90 to 4.63 of a 76 degrees swept arrow wing model with variations in horizontal-tail height, wing height, and dihedral
Year: 1967
Abstract: Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability characteristics of 76 deg swept arrow wing aircraft model
Subject: AIRCRAFT
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:20:24Z | |
| date available | 2017-09-04T15:20:24Z | |
| date copyright | 01/01/1967 | |
| date issued | 1967 | |
| identifier other | ASYKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/20301 | |
| description abstract | Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability characteristics of 76 deg swept arrow wing aircraft model | |
| language | English | |
| title | NASA-TN-D-4076 | num |
| title | Static stability characteristics at Mach numbers from 1.90 to 4.63 of a 76 degrees swept arrow wing model with variations in horizontal-tail height, wing height, and dihedral | en |
| type | standard | |
| page | 119 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1967 | |
| contenttype | fulltext | |
| subject keywords | AIRCRAFT | |
| subject keywords | ANGLE | |
| subject keywords | ARROW | |
| subject keywords | ATTACK | |
| subject keywords | DIHEDRAL | |
| subject keywords | EFFECT | |
| subject keywords | HORIZONTAL | |
| subject keywords | LATERAL | |
| subject keywords | LONGITUDINAL | |
| subject keywords | MACH | |
| subject keywords | MODEL | |
| subject keywords | MODELS | |
| subject keywords | NONLINEARITY | |
| subject keywords | NUMBER | |
| subject keywords | SIDESLIP | |
| subject keywords | STABILITY | |
| subject keywords | STATIC | |
| subject keywords | SURFACES | |
| subject keywords | SWEPT | |
| subject keywords | TAIL | |
| subject keywords | WING | |
| subject keywords | WINGS |