Experimental investigation of a conservatively designed turbine at four rotor-blade solidities Metadata

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Title

  • Main Title Experimental investigation of a conservatively designed turbine at four rotor-blade solidities
  • Series Title NACA Research Memorandums

Creator

  • Author: Heller, Jack A.
    Creator Type: Personal
  • Author: Whitney, Rose L.
    Creator Type: Personal
  • Author: Cavicchi, Richard H.
    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: 1952-07-17

Language

  • English

Description

  • Content Description: Report presenting a program to determine limiting values of the aerodynamic parameters used in turbine design, which includes a study of several turbine designs suitable for application in current aircraft power plants. In this first report, the performance of a single-stage turbine of conservative design was studied for the purpose of establishing a basis for the comparison of turbine performance of less conservative designs.
  • Physical Description: 25 p. : ill.

Subject

  • Keyword: aerodynamics
  • Keyword: turbine design
  • Keyword: turbine performance
  • Keyword: aircraft turbines

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: 93R16403
  • URL: http://hdl.handle.net/2060/19930087113
  • Report No.: NACA-RM-E52C17
  • Center for AeroSpace Information Number: 19930087113
  • Archival Resource Key: ark:/67531/metadc59238