Full-scale wind-tunnel tests of a propeller with the diameter changed by cutting off the blade tips

One of 1,423 reports in the series: NACA Technical Reports available on this site.

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Description

Tests were conducted in order to determine how the characteristics of a propeller are affected by cutting off the tips. The diameter of a standard 10-foot metal propeller was changed successively to 9 feet 6 inches, 9 feet 0 inches, 8 feet 6 inches, and 8 feet 0 inches. Each propeller thus formed was tested at four pitch settings using an open cockpit fuselage and a D-12 engine. A small loss in propulsive efficiency is indicated. Examples are given showing the application of the results to practical problems.

Physical Description

393 - 417 p. : ill.

Creation Information

Wood, Donald H. December 10, 1929.

Context

This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 367 times, with 5 in the last month. More information about this report can be viewed below.

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  • Main Title: Full-scale wind-tunnel tests of a propeller with the diameter changed by cutting off the blade tips
  • Series Title: NACA Technical Reports

Description

Tests were conducted in order to determine how the characteristics of a propeller are affected by cutting off the tips. The diameter of a standard 10-foot metal propeller was changed successively to 9 feet 6 inches, 9 feet 0 inches, 8 feet 6 inches, and 8 feet 0 inches. Each propeller thus formed was tested at four pitch settings using an open cockpit fuselage and a D-12 engine. A small loss in propulsive efficiency is indicated. Examples are given showing the application of the results to practical problems.

Physical Description

393 - 417 p. : ill.

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Identifier

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  • Accession or Local Control No: 93R20709
  • URL: http://hdl.handle.net/2060/19930091419 External Link
  • Report No.: NACA-TR-351
  • Center for AeroSpace Information Number: 19930091419
  • Archival Resource Key: ark:/67531/metadc66003

Collections

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National Advisory Committee for Aeronautics Collection

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).

Technical Report Archive and Image Library

The Technical Report Archive & Image Library (TRAIL) identifies, acquires, catalogs, digitizes and provides unrestricted access to U.S. government agency technical reports. The mission of TRAIL is to ensure preservation, discoverability, and persistent open access to government technical publications regardless of form or format.

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Creation Date

  • December 10, 1929

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • March 13, 2019, 3:01 p.m.

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Wood, Donald H. Full-scale wind-tunnel tests of a propeller with the diameter changed by cutting off the blade tips, report, December 10, 1929; (https://digital.library.unt.edu/ark:/67531/metadc66003/: accessed August 11, 2026), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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