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Investigation of a Dual Propeller at High-Subsonic Mach NumbersAt the present time the Langley 8-foot high-speed tunnel is testing a dual-rotating propeller having a total of eight blades. The front and rear propellers, each made up of four blades, turn in opposite directions. This propeller is designed for a very high blade angle, about 75 degrees, the object being to achieve good efficiency at high forward Mach numbers by means of a low rotational speed so that the resultant Mach numbers along the blade are only slightly greater than the forward Mach number. The design value of advance ratio V/nD is high, about 7.1, so that the tip Mach number is only 10 percent higher than the forward Mach number.
Document ID
19650074081
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Robert J Platt, Jr.
(Langley Research Center Hampton, United States)
Jean Gilman, Jr.
(Langley Research Center Hampton, United States)
Date Acquired
August 2, 2013
Publication Date
September 27, 1949
Publication Information
Publication: NACA Conference on Aerodynamic Problems of Transonic Airplane Design
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-56649
Meeting Information
Meeting: NACA Conference on Aerodynamic Problems of Transonic Airplane Design
Location: Hampton, VA
Country: US
Start Date: September 27, 1949
End Date: September 29, 1949
Sponsors: National Advisory Committee for Aeronautics
Accession Number
65N86484
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
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