Fuselage Torsion of a CT4 Aircraft.

Abstract

The fuselage torsion mode of a CT4 aircraft has been examined using an impulsive testing technique. The mode shape and natural frequency are presented. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1983
Accession Number
ADA142753

Entities

People

  • A. Goldman
  • P. M. Cox

Tags

DTIC Thesaurus Topics

  • Accelerometers
  • Air Force
  • Aircrafts
  • Control Surfaces
  • Defense Industry
  • Department Of Defense
  • Frequency
  • Fuselages
  • Leading Edges
  • Measurement
  • Resonant Frequency
  • Spectrum Analyzers
  • Tape Recorders
  • Test Methods
  • Transfer Functions
  • Vibration
  • Wing Tips

Fields of Study

  • Physics