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Expressions for Measuring the Accuracy of Approximate Solutions to Compressible Flow Through Cascades of Blades With Examples of Use Metadata

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Title

  • Main Title Expressions for Measuring the Accuracy of Approximate Solutions to Compressible Flow Through Cascades of Blades With Examples of Use
  • Series Title NACA Technical Notes

Creator

  • Author: Sinnette, John T., Jr.
    Creator Type: Personal
  • Author: Costello, George R.
    Creator Type: Personal
  • Author: Cummings, Robert L.
    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: 1951-10

Language

  • English

Description

  • Content Description: Report presenting four necessary conditions for steady irrotational compressible flow through a straight cascade of blades as derived from the irrotationality condition and conservation of mass and momentum. The expressions used can only give an approximate solution to the conditions, as there are an infinite number of them.
  • Physical Description: 33 p. : ill.

Subject

  • Keyword: aerodynamics
  • Keyword: flow compressibility

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: 93R12710
  • URL: http://hdl.handle.net/2060/19930083420
  • Report No.: NACA-TN-2501
  • Center for AeroSpace Information Number: 19930083420
  • Archival Resource Key: ark:/67531/metadc56232
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