RESEARCH ON PHYSICAL AND CHEMICAL PRINCIPLES AFFECTING HIGH TEMPERATURE MATERIALS FOR ROCKET NOZZZLES.

Abstract

Data were obtained on the corrosion of W by CO2/Ar mixtures with CO2 stagnation partial pressures of 40, 81, 122, 192, and 340 torr at 2325-3000 K and 340-torr total stagnation pressure. The reaction rate is linear with time. At the lower temperatures log rate is nearly linear with reciprocal temperature for all CO2 partial pressures, and near 3000 K the rates approach those calculated for diffusion control. These data on the CO2-W reaction have been analyzed in terms of an approximate forward rate expression for the surface controlled region, a mass-transfer treatment, and an assumed reverse reaction. The calculated curves agree well with the experimental data, although some questions remain to be resolved; measurements have been made of the corrosion rates of tungsten in mixtures of CO2, CO, and Ar to help clarify these points. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 30, 1964
Accession Number
AD0448483

Entities

People

  • Robert Lowrie

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Chemical Analysis
  • Chemical Engineering
  • Chemistry
  • Composite Materials
  • Crystal Structure
  • Gas Turbine Nozzles
  • Material Degradation Processes
  • Materials
  • Materials Engineering
  • Materials Processing
  • Materials Science
  • Measurement
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Modulus Of Elasticity

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Plasma Physics.
  • Regression Analysis.