Experiments on the design of intake bell for a wind tunnel (airplane section report)

Metadata Field	Value	Language
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

Files in this item