Metal Matrix Composites for High Temperature Application.

Abstract

The objective of the program is to develop fabrication techniques and to characterize high strength-high temperature filament reinforced superalloys for application as turbine blade materials. Using the sessile drop and infiltration techniques, the compatibility of W and SiC filaments against castable superalloys including Mar M200, Mar M302, Mar M322, J-1650, and IN-100 was investigated. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1971
Accession Number
AD0734304

Entities

People

  • Iqbal Ahmad
  • J. M. Barranco
  • K. E. Loomis
  • W. J. Heffernan

Tags

DTIC Thesaurus Topics

  • Advanced Materials
  • Composite Material Fabrication
  • Composite Materials
  • Fabrication
  • Filaments
  • High Temperature
  • Material Forming Processes
  • Materials
  • Materials Processing
  • Metal Matrix Composites
  • Superalloys
  • Turbine Blades
  • Turbines

Fields of Study

  • Materials science

Readers

  • Astronomy and Astrophysics.
  • Powder metallurgy of Titanium alloys.
  • Reinforced Composite Materials