Resonance Tests on a Piper PA-32R Tailplane Before and After Damage.

Abstract

Investigations have been carried out, on the tailplane of a Piper PA-32R aircraft, to determine the effect of damage, in the form of a split in the underside skin, on the modes of vibration of the tailplane. Details and results of the investigations are described. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1981
Accession Number
ADA106273

Entities

People

  • A. Goldman
  • B. Quinn

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accelerometers
  • Air Force
  • Aircrafts
  • Australia
  • Control Surfaces
  • Department Of Defense
  • Frequency
  • Horizontal Stabilizers
  • Leading Edges
  • Measurement
  • Mechanical Waves
  • Motion
  • Resonance
  • Resonant Frequency
  • Surfaces
  • Trailing Edges
  • Vibration

Readers

  • Aerodynamics/Aeronautics.
  • Rocket Propulsion.
  • Structural Dynamics.