dc.creator | Burrows, F. M. | |
dc.date | 2016-03-31T08:22:02Z | |
dc.date | 2016-03-31T08:22:02Z | |
dc.date | 1956-01 | |
dc.date.accessioned | 2022-05-09T10:07:01Z | |
dc.date.available | 2022-05-09T10:07:01Z | |
dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/9805 | |
dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4380 | |
dc.description | 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. | |
dc.language | en | |
dc.publisher | College of Aeronautics | |
dc.relation | CoA/N-36 | |
dc.relation | 36 | |
dc.title | The characteristics of the flow field over the mid-upper fuselage of Lancaster P. A. 474 | |
dc.type | Report |
Files | Size | Format | View |
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COA_N_36_1956.pdf | 4.017Mb | application/pdf |
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