NASA-TM-X-2163
Some transonic and supersonic dynamic stability characteristics of a variable-sweep-wing tactical fighter model
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:34:08Z | |
| date available | 2017-09-04T17:34:08Z | |
| date copyright | 01/01/1971 | |
| date issued | 1971 | |
| identifier other | DENKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/157013 | |
| description abstract | Transonic and supersonic dynamic stability characteristics of variable sweep wing tactical fighter aircraft | |
| language | English | |
| title | NASA-TM-X-2163 | num |
| title | Some transonic and supersonic dynamic stability characteristics of a variable-sweep-wing tactical fighter model | en |
| type | standard | |
| page | 47 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1971 | |
| contenttype | fulltext | |
| subject keywords | AIRCRAFT | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | DYNAMIC | |
| subject keywords | FIGHTER | |
| subject keywords | FLOW | |
| subject keywords | MACH | |
| subject keywords | MODELS | |
| subject keywords | NUMBER | |
| subject keywords | STABILITY | |
| subject keywords | SUPERSONIC | |
| subject keywords | SWEEP | |
| subject keywords | TESTS | |
| subject keywords | TRANSONIC | |
| subject keywords | TUNNEL | |
| subject keywords | VARIABLE | |
| subject keywords | WIND | |
| subject keywords | WINGS |

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