EFFECT OF NOZZLE SECONDARY FLOWS ON TURBINE PERFORMANCE AS INDICATED BY EXIT SURVEYS OF A ROTOR

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Document Details

Document Type
Technical Report
Publication Date
Apr 05, 1954
Accession Number
AD0030156

Entities

People

  • Daniel E. Monroe
  • Howard A. Buckner Jr.
  • Warren J. Whitney

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Efficiency
  • Flow
  • Government Procurement
  • Governments
  • Hot Wire Anemometers
  • Instrumentation
  • Mach Number
  • Mass
  • Mass Flow
  • Measurement
  • National Security
  • Pressure Gradients
  • Secondary Flow
  • Static Pressure
  • Thermocouples
  • Vortices