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dc.creatorUnited States. Army. Air Service. Engineering Division.en_US
dc.date.accessioned2018-07-31T13:55:14Z
dc.date.available2018-07-31T13:55:14Z
dc.date.created1921-04-30en_US
dc.identifier.urihttp://hdl.handle.net/11200/49186
dc.descriptionIn 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.formatPDFen_US
dc.publisherWashington, D.C. : Chief of Air Serviceen_US
dc.relation.ispartofseriesAir Service information circular (Aviation) ; v. 3, no. 217en_US
dc.relation.ispartofseriesMcCook Field report ; Serial no. 1441en_US
dc.subjectWind tunnels--Design and constructionen_US
dc.subjectWind tunnels--Testingen_US
dc.titleExperiments on the design of intake bell for a wind tunnel (airplane section report)en_US
dc.typeTexten_US


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