A Method of Designing Turbomachine Blades with a Desirable Thickness Distribution for Compressible Flow Along an Arbitrary Stream Filament of Revolution

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1951
Accession Number
ADA380473

Entities

People

  • Chung-hua Wu
  • Curtis A. Brown

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Accuracy
  • Axial Flow
  • Centrifugal Compressors
  • Compressible Flow
  • Flow
  • Fluid Flow
  • Incompressible Flow
  • Inverse Problems
  • Mach Number
  • Mass Flow
  • Power Series
  • Radial Flow
  • Shape
  • Streamline Shape
  • Trailing Edges
  • Turbine Blades
  • Two Dimensional