Investigation of a 0.6 Hub-Tip Radius-Ratio Transonic Turbine Designed for Secondary-Flow Study 3 - Experimental Performance With Two Stator Configurations Designed to Eliminate Blade Wakes and Secondary-Flow Effects and Conclusions From Entire Stator Investigation Metadata

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Title

  • Main Title Investigation of a 0.6 Hub-Tip Radius-Ratio Transonic Turbine Designed for Secondary-Flow Study 3 - Experimental Performance With Two Stator Configurations Designed to Eliminate Blade Wakes and Secondary-Flow Effects and Conclusions From Entire Stator Investigation
  • Series Title NACA Research Memorandums

Creator

  • Author: Rohlik, Harold E.
    Creator Type: Personal
  • Author: Wintucky, William T.
    Creator Type: Personal
  • Author: Moffitt, Thomas P.
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: NASA Lewis Research Center

Date

  • Creation: 1957-09-17

Language

  • English

Description

  • Content Description: Memorandum presenting two turbine stator configurations designed to investigate the effect on turbine performance of either reducing or eliminating stator-blade wakes, secondary-flow loss accumulations, and circumferential variations in total pressure at the stator exits. Results regarding stator surveys, overall performance with the semivaneless stator, overall performance with the standard stator with spacer, rotor-exit surveys, and rotor-blade momentum loss are provided.
  • Physical Description: 27 p. : ill.

Subject

  • Keyword: aircraft turbines
  • Keyword: flow characteristics

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: 63N12546
  • URL: http://hdl.handle.net/2060/19630002670
  • Report No.: NACA-RM-E57G08
  • Center for AeroSpace Information Number: 19630002670
  • Archival Resource Key: ark:/67531/metadc52873

Note

  • Display Note: "III."
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