Computational Design of UHTC Materials for Hypersonic Applications (Preprint)

Abstract

Ultra-High Temperature Ceramics (UHTC) are attractive candidates for use as leading edge components. This work explores the possibility of using computational methods to design a structure of higher strength and toughness within the constraint of 2D isotropy. The use of low-aspect ratio bone-shaped short fibers (BSSF) to improve fracture toughness and the use of composition tailoring to increase fiber strength were analyzed. Computational models show that significant improvements in fracture toughness can be realized with an aspect ratio of 15 if the fiber strengths can be raised to 1.5 GPa. The use of a single outer layer of lower thermal expansivity composition is predicted to increase strength by a factor of two, while multilayers of reasonable thickness result in strengthening by a factor of 3. It is predicted that these designs will offer significant leverage to increments from processing advances. An optimal design for a 2D fibrous monolith UHTC is suggested.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2006
Accession Number
ADA460079

Entities

People

  • Abhishek Roy
  • R. J. Kerans
  • S. Chellapilla
  • Triplicane A. Parthasarathy

Organizations

  • Universal Energy Systems

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Aspect Ratio
  • Ceramic Matrix Composites
  • Composite Materials
  • Computational Science
  • High Temperature
  • Leading Edges
  • Materials
  • Mechanical Properties
  • Mechanics
  • Residual Stress
  • Tensile Stress
  • Thickness
  • Three Dimensional
  • Toughness
  • Two Dimensional

Fields of Study

  • Materials science
  • Physics

Readers

  • Materials Science (Mechanical Engineering).
  • Reinforced Composite Materials

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight