Effect of a Trailing-Edge Extension on the Characteristics of a Propeller Section Metadata

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Title

  • Main Title Effect of a Trailing-Edge Extension on the Characteristics of a Propeller Section
  • Series Title NACA Wartime Reports
  • Series Title NACA Advanced Confidential Reports

Creator

  • Author: Theodorsen, Theodore
    Creator Type: Personal
  • Author: Stickle, George W.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1944-09

Language

  • English

Description

  • Content Description: Report presenting a convenient technical method to evaluate changes in the airfoil characteristics resulting from an extension of the chord at the trailing edge of a propeller blade section. The method determines the change in the angle of zero lift, the ideal angle of attack, and the difference in these angles as a function of the angle and length of the trailing-edge extension.
  • Physical Description: [34] p.

Subject

  • Keyword: aircraft propellers
  • Keyword: trailing-edge extensions

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: 93R22131
  • URL: http://hdl.handle.net/2060/19930092841
  • Report No.: NACA-WR-L-637
  • Report No.: NACA-ACR-L4I21
  • Center for AeroSpace Information Number: 19930092841
  • Archival Resource Key: ark:/67531/metadc61477