Aerodynamic Characteristics in the Approach, Superfine and Negative Pitch Ranges of Two Four-Bladed Propellers with N.A.C.A. Series 16 Blade Sections.

dc.contributor.author	Technical Staffs of de Havilland Propellers	en_US
dc.contributor.author	Limited	en_US
dc.contributor.author	Rotol	en_US
dc.contributor.author	Limited.	en_US
dc.date.accessioned	2014-10-21T15:54:43Z
dc.date.available	2014-10-21T15:54:43Z
dc.date.issued	1957	en_US
dc.identifier.other	ARC/R&M-3105	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3676
dc.description.abstract	Tests were conducted on two similar full-scale propellers in tim 24-ft Wind Tunnel at the Royal Aircraft Establishment by representatives of Rotol, Ltd. and de Havilland Propellers, Ltd. to measure the aerodynamic characteristics over a blade-angle range of - 20 deg to + 40 deg, measured at the 0.7 radius, and over a range of advance ratio of 0.1 to 2.4.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Aerodynamic Characteristics in the Approach, Superfine and Negative Pitch Ranges of Two Four-Bladed Propellers with N.A.C.A. Series 16 Blade Sections.	en_US