The characteristics of the flow field over the mid-upper fuselage of Lancaster P. A. 474
dc.contributor.author | Burrows, F. M. | |
dc.date.accessioned | 2016-03-31T08:22:02Z | |
dc.date.available | 2016-03-31T08:22:02Z | |
dc.date.issued | 1956-01 | |
dc.description.abstract | This 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.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/9805 | |
dc.language.iso | en | en_UK |
dc.publisher | College of Aeronautics | en_UK |
dc.relation.ispartofseries | CoA/N-36 | en_UK |
dc.relation.ispartofseries | 36 | en_UK |
dc.title | The characteristics of the flow field over the mid-upper fuselage of Lancaster P. A. 474 | en_UK |
dc.type | Report | en_UK |