Analysis of spanwise temperature distribution in three types of air-cooled turbine blade Metadata

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Title

  • Main Title Analysis of spanwise temperature distribution in three types of air-cooled turbine blade
  • Series Title NACA Technical Reports

Creator

  • Author: Livingood, John N. B.
    Creator Type: Personal
  • Author: Brown, W. Byron
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab

Date

  • Creation: 1950-03-01

Language

  • English

Description

  • Content Description: From Summary: An approximate method for determining the allowable stress-limited blade-temperature distribution is included, with brief accounts of a method for determining the maximum allowable effective gas temperatures and the cooling-air requirements. Numerical examples that illustrate the use of the various temperature-distribution equations and of the nondimensional charts are also included.
  • Physical Description: 18 p. : ill.

Subject

  • Keyword: blades
  • Keyword: methods

Coverage

  • Coverage Date: 1949

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: 93R21342
  • URL: http://hdl.handle.net/2060/19930092052
  • Report No.: NACA-TR-994
  • Center for AeroSpace Information Number: 19930092052
  • Archival Resource Key: ark:/67531/metadc60333
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