Damage Resistance Characterization of Sandwich Composites Using Response Surfaces

Abstract

The influence of material configuration and impact parameters on the damage-resistance characteristics of sandwich composites comprised of carbon-epoxy woven fabric facesheets and Nomex honeycomb cores were investigated using empirically based response surfaces. A series of carefully selected tests were used to isolate the coupled influence of number of facesheet plies, core density, core thickness, impact energy, impactor diameter, and impact velocity on the damage formation due to impact normal to the surface. The ranges of selected material parameters were typical of those found in common aircraft applications. The diameter of the planar damage area, which was determined using through transmission ultrasonic (TTU) C-scan measurements and the maximum residual facesheet indentation depth, was used to describe the extent of internal and detectable surface damage, respectively. Estimates of the size of the planar damage region as a function of material system and impact parameters made using quadratic response surface correlated reasonably well with experimentally determined values. For a fixed set of impact parameters, estimates of the planar damage size and residual facesheet indentation suggest that impact damage is highly dependent on skin thickness and core density and thickness. Increasing the thickness of core and decreasing the number of facesheet plies generally resulted in the greatest reduction in the estimated planar damage dimension while increasing the amount of facesheet indentation. An increase in the impactor diameter results in a significant increase in the estimated planar damage size and a decrease in the residual facesheet indentation, particularly for those sandwich panels with thicker facesheets. Thus, blunt object impacts result in appreciable damage that is not detectable using visual inspection. The effects of impact energy and velocity on damage formation were also addressed.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2002
Accession Number
ADA401607

Entities

People

  • I. K. Samarah
  • J. S. Tomblin
  • T. E. Lacy

Organizations

  • Wichita State University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Applied Mechanics
  • Composite Materials
  • Damage Tolerance
  • Energy Levels
  • Experimental Data
  • Experimental Design
  • Honeycomb Cores
  • Laminates
  • Materials
  • Mechanics
  • Regression Analysis
  • Sandwich Composites
  • Sandwich Panels
  • Two Dimensional
  • Visual Inspection

Fields of Study

  • Materials science

Readers

  • Mathematics or Statistics
  • Structural Health Monitoring of Composite Structures.