STRUCTURAL ANALYSIS WING BASIC COMPONENTS

Abstract

The structural analysis of the basic wing components of the U. S. Army XV-5A Lift Fan Research Aircraft is presented. The basic structural components of the wing are composed of the two spars, the wing leading edge torque box, and the skins and ribs of the panel outboard of the lift fan. A complete digital computer program applicable to this and other highly redundant structures was developed. Since this program was used in the structural analysis and design, the deflections, internal loads, and internal stresses for critical flight conditions are summarized in the form of printed computer output.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1963
Accession Number
AD0653565

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Bolts
  • Computer Programs
  • Computers
  • Digital Computers
  • Geometry
  • High Angles
  • Lift Fans
  • Low Angles
  • Oils
  • Research Aircraft
  • Shear Flow
  • Spars
  • Stress Analysis
  • Structural Analysis
  • Structural Components
  • Tank Guns

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Structural Dynamics.