The characteristics of the flow field over the mid-upper fuselage of Lancaster P. A. 474

dc.contributor.authorBurrows, F. M.
dc.date.accessioned2016-03-31T08:22:02Z
dc.date.available2016-03-31T08:22:02Z
dc.date.issued1956-01
dc.description.abstractThis note describes a series of tests conducted to determine the characteristics of the flow field over the mid-upper fuselage of. Lancaster P. A, 474. The range of the tests was to include a determination of the distributions of total head, static pressure and velocity together with the flow directional characteristics in the pitching plane for a number of aircraft flight configurations as listed in paragraph 1. 2. Curves are presented in Figs. 9, 20 - 25, showing the flow directional characteristics and the distributions of static pressure and velocity in the region of investigation.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/9805
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N-36en_UK
dc.relation.ispartofseries36en_UK
dc.titleThe characteristics of the flow field over the mid-upper fuselage of Lancaster P. A. 474en_UK
dc.typeReporten_UK

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