The application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory Metadata

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Title

  • Main Title The application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory
  • Series Title NACA Technical Reports

Creator

  • Author: Heaslet, Max A.
    Creator Type: Personal
  • Author: Lomax, Harvard
    Creator Type: Personal

Contributor

  • Originator: Ames Aeronautical Laboratory (U.S.)
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab

Date

  • Creation: 1948-12-22

Language

  • English

Description

  • Content Description: From Introduction: "The present paper is restricted to a discussion of wing theory subject to the assumptions of linearized compressible flow. It therefore employs solutions of Laplace's equation and the wave equation for cases where the boundary condition are specified in the plane of the wing."
  • Physical Description: 14 p. : ill.

Subject

  • Keyword: Green's Theorem
  • Keyword: wings

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: 93R21314
  • URL: http://hdl.handle.net/2060/19930092024
  • Report No.: NACA-TR-961
  • Center for AeroSpace Information Number: 19930092024
  • Archival Resource Key: ark:/67531/metadc60293
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