Effects of Interstage Diffuser Flow Distortion on the Performance of a 15.41-Centimeter Tip Diameter Axial Power Turbine.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1983
Accession Number
ADA130296

Entities

People

  • Kerry L. Mclallin
  • Kestutis C. Civinskas
  • Milton G. Kofskey

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Axial Flow
  • Boundary Layer
  • Flow
  • Flow Rate
  • Fluid Dynamics
  • Fluid Mechanics
  • Gas Turbines
  • Governments
  • Instrumentation
  • Mass Flow
  • Measurement
  • Research Facilities
  • Static Pressure
  • Turbine Components
  • Turbines
  • United States
  • United States Government