Vibratory-stress investigation of six- and eight-blade-dual-rotating propellers operating at zero advance Metadata

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Title

  • Main Title Vibratory-stress investigation of six- and eight-blade-dual-rotating propellers operating at zero advance
  • Series Title NACA Research Memorandums

Creator

  • Author: Heath, Atwood R., Jr.
    Creator Type: Personal
  • Author: O'Neal, Robert L.
    Creator Type: Personal

Contributor

  • Originator: Langley Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab

Date

  • Creation: 1955-02-04

Language

  • English

Description

  • Content Description: Report presenting the results of an investigation of the vibratory stresses of a dual-rotating propeller with both six-blade and eight-blade configurations using the NACA 6,000-horsepower propeller dynamometer. Attention was focused on the measurement of vibratory stresses caused by mutual blade interference of the front- and rear-propeller components. A range of blade angles and rotational speeds were used in testing.

Subject

  • Keyword: aircraft propellers
  • Keyword: vibratory stresses
  • Keyword: dual-rotating propellers

Collection

  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL

Institution

  • Name: UNT Libraries Government Documents Department
    Code: 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: 93R17734
  • URL: http://hdl.handle.net/2060/19930088444
  • Report No.: NACA-RM-L54J28
  • Center for AeroSpace Information Number: 19930088444
  • Archival Resource Key: ark:/67531/metadc60870