Investigation of the Sonic Fatigue Characteristics of Randomly Excited Aluminum Viscoelastic Panels at Ambient Temperatures

Abstract

An experimental sonic fatigue program was conducted on aluminum viscoelastic and aluminum control panels. The panels were tested at 154 db, 157 db, and 160 db using a Broad-Band Siren as the noise source. Previously, these structures were evaluated under discrete frequency excitation. The primary purpose of this effort was to continue to investigate the usefulness of viscoelastic structures under high acoustic random loads. Tests substantiate that the viscoelastic panel has slightly better sonic fatigue properties than an equivalent-by-weight aluminum panel.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1966
Accession Number
ADA374201

Entities

People

  • B. J. Moskal

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acquisition
  • Aircrafts
  • Analyzers
  • Bandwidth
  • Coefficients
  • Control Panels
  • Data Acquisition
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Frequency
  • Measurement
  • Modal Analysis
  • Modulus Of Elasticity
  • Recording Systems
  • Sonic Fatigue
  • Sound Pressure
  • Strain Gages

Fields of Study

  • Physics

Readers

  • Defense Technology Research and Development.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Mechanical Engineering/Mechanics of Materials.