Methods and Formulas for Calculating the Strength of Plate and Shell Constructions as Used in Airplane Design Metadata

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Title

  • Main Title Methods and Formulas for Calculating the Strength of Plate and Shell Constructions as Used in Airplane Design
  • Series Title NACA Technical Memorandums

Creator

  • Author: Heck, O. S.
    Creator Type: Personal
  • Author: Ebner, H.
    Creator Type: Personal

Contributor

  • Originator: United States. National Advisory Committee for Aeronautics.
    Contributor Type: Organization

Date

  • Creation: 1936-02

Language

  • English

Description

  • Content Description: "This report is a compilation of previously published articles on formulas and methods of calculation for the determination of the strength and stability of plate and shell construction as employed in airplane design. In particular, it treats the problem of isotropic, orthotopic, and stiffened rectangular plates, thin curved panels, and circular cylinders under various loading conditions. The purpose of appending the pertinent literature references following the subjects discussed was to facilitate a comprehensive study of the treated problems" (p. 1).
  • Physical Description: [46] p. : ill.

Subject

  • Keyword: aircraft design
  • Keyword: plate construction
  • Keyword: shell construction

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: 93R23552
  • URL: http://hdl.handle.net/2060/19930094632
  • Report No.: NACA-TM-785
  • Center for AeroSpace Information Number: 19930094632
  • Archival Resource Key: ark:/67531/metadc63430
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