DEVELOPMENT OF RESISTANCE STRAIN GAGES USABLE UP TO 1600 F

Abstract

To measure stresses produced in aircraft structures by aerodynamic heating, a quasi-static high temperature strain gage is required which exhibits good stability characteristics. In the present application it was desired to measure large strains in the temperature range 1000 to 1600 F. Refractory single phase alloys with Fe, Co, and Ni bases were selected for exploration as strain gage wires. Besides good oxidation resistance it was aimed to achieve a low temperature coefficient of resistance and matching expansivity with the chosen base material. The solid solution alloys of the Fe-Cr-Al composition approached most closely the ideal requirements for high temperature strain gage wires. Several alloys in this group were vacuum melted and the hot and cold forming properties were determined. Fe25 Cr-5 Al, Fe-25 Cr-7.5 Al, and Fe-20 Cr-10 Al alloys ultimately were drawn into 0.001 to 0.002in.-diam wires. Strain gages fabricated from these wires were cemented to Inconel test bars and preliminary gage calibrations were made at elevated temperatures. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 23, 1962
Accession Number
AD0273322

Entities

People

  • G. Stevens
  • J.p. Sheehan

Organizations

  • IIT Research Institute

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Alloys
  • Coefficients
  • Cold Working
  • Gages
  • High Temperature
  • Low Temperature
  • Materials
  • Materials Processing
  • Oxidation
  • Oxidation Resistance
  • Resistance
  • Solid Solutions
  • Strain Gages
  • Temperature Coefficients

Fields of Study

  • Materials science

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Metallurgy
  • Powder metallurgy of Titanium alloys.