24-ft wind tunnel tests on a propeller with NACA 16 series sections. Test results and analysis into mean lift-drag data

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