Wind-Tunnel Tests of a Dual-Rotating Propeller Having One Component Locked or Windmilling Metadata
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Title
- Main Title Wind-Tunnel Tests of a Dual-Rotating Propeller Having One Component Locked or Windmilling
- Series Title NACA Wartime Reports
- Series Title NACA Advanced Restricted Reports
Creator
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Author: Bartlett, Walter A., Jr.Creator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
Date
- Creation: 1945-01
Language
- English
Description
- Content Description: "The effect on the propulsive efficiency of locking or windmilling one propeller of a six-blade dual-rotating propeller installation was determined in the Langley propeller-research tunnel. Tests were made of both pusher and tractor configurations, with the unpowered propeller both leading and following the powered propeller, which was set at a blade angle of 40 degrees. The maximum propulsive efficiency of the powered propeller in combination with the locked or windmilling propeller was, in all cases, lower than that of the powered propeller operating alone" (p. 1).
- Physical Description: [26] p. : ill.
Subject
- Keyword: aerodynamics
- Keyword: propellers
- Keyword: dual-rotating propellers
Collection
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Name: National Advisory Committee for Aeronautics CollectionCode: NACA
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Name: Technical Report Archive and Image LibraryCode: TRAIL
Institution
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Name: UNT Libraries Government Documents DepartmentCode: UNTGD
Rights
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
Resource Type
- Report
Format
- Text
Identifier
- Accession or Local Control No: 93R22629
- URL: http://hdl.handle.net/2060/19930093339
- Report No.: NACA-WR-L-214
- Report No.: NACA-ARR-L5A13a
- Center for AeroSpace Information Number: 19930093339
- Archival Resource Key: ark:/67531/metadc62184