درباره ما
NACA-TM-1122
Systematic Wind-Tunnel Measurements on Missiles
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:31:00Z | |
| date available | 2017-09-04T17:31:00Z | |
| date copyright | 01/01/1947 | |
| date issued | 1947 | |
| identifier other | CWITDEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/153949 | |
| description abstract | Wind-tunnel measurements on projectiles are discussed. Tests at the Gottingen Tunnel are described. The tunnel operates on the Prandtl principle, that is, a brief stationary air stream produced in an evacuated tank by induction of atmospheric air. | |
| language | English | |
| title | NACA-TM-1122 | num |
| title | Systematic Wind-Tunnel Measurements on Missiles | en |
| type | standard | |
| page | 24 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext | |
| subject keywords | AIR | |
| subject keywords | ANGLE | |
| subject keywords | ATTACK | |
| subject keywords | FLOW | |
| subject keywords | MATHEMATICAL | |
| subject keywords | MISSILES | |
| subject keywords | MODELS | |
| subject keywords | PROJECTILES | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND |
