The flow at the mouth of a stanton pitot

Show simple item record A. Thom en_US 2014-10-21T15:54:06Z 2014-10-21T15:54:06Z 1952 en_US
dc.identifier.other ARC/R&M-2984 en_US
dc.description.abstract An arithmetical calculation is made of the flow at the mouth of a Stanton Pitot as the Reynolds number tends to zero. A stationary eddy is found under the lip of the Pitot. A figure is found for the height of the effective centre of the Pitot rather greater than the experimental value determined by Sir Geoffrey Taylor. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The flow at the mouth of a stanton pitot en_US

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