Hostname: page-component-cd9895bd7-jkksz Total loading time: 0 Render date: 2024-12-25T06:32:07.993Z Has data issue: false hasContentIssue false

Viscous Effects on Flattened Pitot Tubes at Low Speeds

Published online by Cambridge University Press:  28 July 2016

F. A. Macmillan*
Affiliation:
Engineering Laboratory, University of Cambridge

Extract

Measurements were made of the pressures in flattened, blunt-nosed pitot tubes, in an air stream at Reynolds numbers from 13-1,000 (based on the external height of the tube). Three tubes were used, having cross sections with ratios of width to height (W/H) of 3, 7 and 11.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1954

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. MacMillan, F. A. 1954. Viscous Effects on Pitot Tubes at Low Speeds. Journal of the Royal Aeronautical Society, Vol. 58, pp. 570572, 1954.CrossRefGoogle Scholar