dc.contributor.author |
A. R. C. MacDougall |
en_US |
dc.contributor.author |
A. B. Haines |
en_US |
dc.date.accessioned |
2014-10-21T15:51:45Z |
|
dc.date.available |
2014-10-21T15:51:45Z |
|
dc.date.issued |
1948 |
en_US |
dc.identifier.other |
ARC/R&M-2602 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3139 |
|
dc.description.abstract |
This report gives the results of tests made in the Royal Aircraft Establishment 24-ft Wind Tunnel on the de Havilland propeller for the Aeronautical Research Council research programme initiated in 1943. The propeller was designed to give a good performance at high forward speeds and the aim of these tests was to check whether, as a result, serious losses in take-off performance had been incurred. The results are more reassuring than was expected. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
24-ft wind tunnel tests on a propeller with NACA 16 series sections. Test results and analysis into mean lift-drag data |
en_US |