STRUCTURAL ANALYSIS OF WING SECONDARY COMPONENTS

Abstract

Structural Analysis of the flap, aileron, wing fan closure doors, wing trailing edge, and wing fittings for the U.S. Army XV-5A lift fan research aircraft are presented in this report. For each component, a summary type analysis is presented primarily with the intent of giving structural configuration, final critical loading, and assumptions made. Structural proof tests were conducted satisfactorily on the basic wing, the fan doors, fan fittings, flap and aileron.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1963
Accession Number
AD0636574

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Actuators
  • Aircrafts
  • Army Aviation
  • Cells
  • Department Of Defense
  • Flight
  • Fuselages
  • Government (Foreign)
  • Government Procurement
  • Governments
  • Ions
  • Lift Fans
  • Pressure Distribution
  • Research Aircraft
  • Spars
  • Structural Analysis
  • Trailing Edges

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Structural Health Monitoring of Composite Structures.