GAS-TO-BLADE HEAT-TRANSFER COEFFICIENTS AND TURBINE HEAT-REJECTION RATES FOR A RANGE OF ONE-SPOOL COOLED-TURBINE ENGINE DESIGNS

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Document Details

Document Type
Technical Report
Publication Date
May 14, 1956
Accession Number
AD0094052

Entities

People

  • Henry O. Slone
  • Jack B. Esgar

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Cooled
  • Aspect Ratio
  • Diameters
  • Engines
  • Equations
  • Government Procurement
  • Governments
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mach Number
  • Sea Level
  • Temperature Gradients
  • Turbine Blades
  • Turbine Stators
  • Turbines
  • Turbojet Engines
  • Turboprop Engines