| dc.creator | United States. Army. Air Service. Engineering Division. | en_US |
| dc.date.accessioned | 2018-07-31T13:55:14Z | |
| dc.date.available | 2018-07-31T13:55:14Z | |
| dc.date.created | 1921-04-30 | en_US |
| dc.identifier.uri | http://hdl.handle.net/11200/49186 | |
| dc.description | In order to investigate the effect of the intake bell on the smoothness of flow in a wind tunnel, a series of experiments were made September 27--October 3, 1919, in which four types of intake bell were tried out on a model wind tunnel. The conclusion reached is that the Grimes type intake bell gives the best velocity distribution, same being practically constant over 93 per cent of the diameter. | en_US |
| dc.format | PDF | en_US |
| dc.publisher | Washington, D.C. : Chief of Air Service | en_US |
| dc.relation.ispartofseries | Air Service information circular (Aviation) ; v. 3, no. 217 | en_US |
| dc.relation.ispartofseries | McCook Field report ; Serial no. 1441 | en_US |
| dc.subject | Wind tunnels--Design and construction | en_US |
| dc.subject | Wind tunnels--Testing | en_US |
| dc.title | Experiments on the design of intake bell for a wind tunnel (airplane section report) | en_US |
| dc.type | Text | en_US |
