A Solution of the Direct and Inverse Potential Problems for Arbitrary Cascades of Airfoils Metadata

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Title

  • Main Title A Solution of the Direct and Inverse Potential Problems for Arbitrary Cascades of Airfoils
  • Series Title NACA Wartime Reports
  • Series Title NACA Advanced Restricted Reports

Creator

  • Author: Mutterperl, William
    Creator Type: Personal

Contributor

  • Originator: Langley Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab

Date

  • Creation: 1944-12

Language

  • English

Description

  • Content Description: Methods are given of determining the potential flow plast an arbitrary cascade of airfoils and the inverse problem of determining an airfoil having a prescribed velocity distribution in cascade. Results indicated that Cartesian mapping function method may be satisfactorily extended to include cascades. Numerical calculation for computing cascades by Cartesian mapping function method is considerably greater than for single airfoils but much less than hitherto required for cascades.
  • Physical Description: [50] p. : ill.

Subject

  • Keyword: airfoils
  • Keyword: airfoil cascades

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: 93R22005
  • URL: http://hdl.handle.net/2060/19930092715
  • Report No.: NACA-WR-L-81
  • Report No.: NACA-ARR-L4K22B
  • Center for AeroSpace Information Number: 19930092715
  • Archival Resource Key: ark:/67531/metadc61263