Sonic Fatigue Design Method for the Response of CFRP (Carbon-Fibre Reinforced Plastic) Stiffened-Skin Panels

Abstract

This paper describes the development of a semi-empirical method to estimate the structural response of cfrp stiffened-skin panels when method suitable for practical use in the design of crfp airplane structures, utilizing the results from previous work.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1984
Accession Number
ADP003707

Entities

People

  • Ian Holehouse

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Aspect Ratio
  • Carbon Fiber Reinforced Polymer
  • Carbon Fibers
  • Computer Programs
  • Curvature
  • Databases
  • Dynamic Response
  • Frequency
  • Information Science
  • Numbers
  • Regression Analysis
  • Resonant Frequency
  • Sonic Fatigue
  • Sound Pressure
  • Structural Response

Fields of Study

  • Materials science

Readers

  • Reinforced Composite Materials
  • Structural Dynamics.