Acoustic Fatigue Design Data, Part 1

Abstract

The report, the first part of a series giving data for design against acoustic fatigue, has been prepared in order to draw together the results of research in acoustic fatigue and to present them in a form directly useable in aerospace design. Future work in this series will deal with endurance of aluminum alloy and titanium alloy structures under simulated acoustic loading, stress response of flat or curved honeycomb panels, near field compressor noise estimation, stress response of box and control surface structures and structural damping.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1972
Accession Number
AD0744210

Entities

People

  • A. G. Thomson

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Boundary Layer
  • Control Surfaces
  • Engine Noise
  • Engineering
  • Frequency
  • Materials
  • Modulus Of Elasticity
  • Nato
  • Near Field
  • Propulsion Systems
  • Resonant Frequency
  • Sound Pressure
  • Stiffness
  • Vibration

Fields of Study

  • Physics

Readers

  • Structural Dynamics.
  • Structural Health Monitoring of Composite Structures.
  • Systems Analysis and Design

Technology Areas

  • Space