COMPARISON OF THEORETICALLY AND EXPERIMENTALLY DETERMINED EFFECTS OF OXIDE COATINGS SUPPLIED BY FUEL ADDITIVES ON UNCOOLED TURBINE-BLADE TEMPERATURE DURING TRANSIENT TURBOJET-ENGINE OPERATION

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 30, 1953
Accession Number
AD0005535

Entities

People

  • Francis S. Stepka
  • Louis J. Schafer Jr.
  • W. B. Brown

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms

DTIC Thesaurus Topics

  • Additives (Chemicals)
  • Boundaries
  • Combustion
  • Differential Equations
  • Equations
  • Fuel Additives
  • Fuel Nozzles
  • Gas Flow
  • Gas Turbines
  • Heat Transfer
  • Heat Transfer Coefficients
  • Heat Transmission
  • Leading Edges
  • Measurement
  • Thermal Conductivity
  • Turbine Blades
  • Turbojet Engines