The Theory of Propellers 3: The Slipstream Contraction With Numerical Values for Two-Blade and Four-Blade Propeller Metadata

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Title

  • Main Title The Theory of Propellers 3: The Slipstream Contraction With Numerical Values for Two-Blade and Four-Blade Propeller
  • Series Title NACA Wartime Reports
  • Series Title NACA Advanced Confidential Reports

Creator

  • Author: Theodorsen, Theodore
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1944-11

Language

  • English

Description

  • Content Description: Report presenting the magnitude of slipstream contraction, which provides information about the conditions of the ultimate wake. Curves and tables are given for the contraction coefficient of two-blade and four-blade propellers for various values of the advance ratio; the contraction coefficient is defined as the contraction in the diameter of the wake helix in terms of the wake diameter at infinity.
  • Physical Description: 75-97 p.

Subject

  • Keyword: aircraft propellers
  • Keyword: slipstream contractions

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: 93R22600
  • URL: http://hdl.handle.net/2060/19930093310
  • Report No.: NACA-WR-L-155
  • Report No.: NACA-ACR-L4J10
  • Center for AeroSpace Information Number: 19930093310
  • Archival Resource Key: ark:/67531/metadc62140

Note

  • Display Note: "III."
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