Comparison of Calculated and Experimental Temperatures and Coolant Pressure Losses for a Cascade of Small Air-Cooled Turbine Rotor Blades

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Document Details

Document Type
Technical Report
Publication Date
Sep 04, 1958
Accession Number
AD0224446

Entities

People

  • Francis S. Stepka

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Cooled
  • Air Pressure
  • Air Temperature
  • Aspect Ratio
  • Combustion
  • Compressors
  • Engines
  • Experimental Data
  • Flow
  • Heat Transfer
  • Heat Transfer Coefficients
  • Static Pressure
  • Temperature Gradients
  • Turbine Blades
  • Turbojet Engines
  • Turboprop Engines
  • Turbulent Flow