درباره ما
NACA-TN-3176
Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds
Year: 1954
Abstract: Linearized compressible-flow analysis is applied to the study of wind-tunnel-wall interference for subsonic flow in either two-dimension or circular test sections having slotted or porous walls. Expressions are developed for evaluating blockage and lift interference.
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:39:56Z | |
| date available | 2017-09-04T18:39:56Z | |
| date copyright | 01/01/1954 | |
| date issued | 1954 | |
| identifier other | JTNUYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/221622 | |
| description abstract | Linearized compressible-flow analysis is applied to the study of wind-tunnel-wall interference for subsonic flow in either two-dimension or circular test sections having slotted or porous walls. Expressions are developed for evaluating blockage and lift interference. | |
| language | English | |
| title | NACA-TN-3176 | num |
| title | Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds | en |
| type | standard | |
| page | 43 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1954 | |
| contenttype | fulltext |