Fuselage stress analysis Metadata

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Title

  • Main Title Fuselage stress analysis
  • Series Title NACA Technical Reports

Creator

  • Author: Warner, Edward P.
    Creator Type: Personal
  • Author: Miller, Roy G.
    Creator Type: Personal

Contributor

  • Originator: Bureau of Construction and Repair (Navy). Aerodynamical Laboratory
    Contributor Type: Organization

Date

  • Creation: 1920-01-01

Language

  • English

Description

  • Content Description: Report analyzes the stresses in a fuselage of the built-up type in which the shear is taken by diagonal bracing wires. Tests are conducted for landing, flying, and thrust loads.

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

  • 93R20427
  • URL: http://hdl.handle.net/2060/19930091137
  • Report No.: NACA-TR-76
  • Center for AeroSpace Information Number: 19930091137
  • Archival Resource Key: ark:/67531/metadc65725