Design and Experimental Performance of a 0.35 Hub-Tip Radius Ratio Transonic Axial-Flow-Compressor Rotor Designed for 40 Pounds Per Second Per Unit Frontal Area Metadata

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Title

  • Main Title Design and Experimental Performance of a 0.35 Hub-Tip Radius Ratio Transonic Axial-Flow-Compressor Rotor Designed for 40 Pounds Per Second Per Unit Frontal Area
  • Series Title NACA Research Memorandums

Creator

  • Author: Montgomery, John C.
    Creator Type: Personal
  • Author: Yasaki, Paul T.
    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: 1958-09-04

Language

  • English

Description

  • Content Description: Memorandum presenting an investigation to determine the feasibility of a high-performance transonic axial-flow compressor stage with a weight flow of 40 pounds per second per square foot of frontal area. A transonic axial-flow inlet stage with a hub-tip ratio of 0.35 and an axial Mach number of approximately 0.75 was designed and fabricated. Results regarding overall rotor performance, flow parameters, radial matching of blade-element sections, and comparison of blade-element parameters with design rules are provided.
  • Physical Description: 39 p. : ill.

Subject

  • Keyword: axial-flow compressors
  • Keyword: aircraft inlets

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: 93R15353
  • URL: http://hdl.handle.net/2060/19930086063
  • Report No.: NACA-RM-E58D17
  • Center for AeroSpace Information Number: 19930086063
  • Archival Resource Key: ark:/67531/metadc58374
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