A Method of Solving the Direct and Inverse Problem of Supersonic Flow Along Arbitrary Stream Filaments of Revolution in Turbomachines

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1951
Accession Number
ADA380598

Entities

People

  • Chung-hua Wu
  • Eleanor L. Costilow

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axial Flow Compressors
  • Boundaries
  • Cartesian Coordinates
  • Curvature
  • Equations
  • Filaments
  • Flow
  • Inverse Problems
  • Leading Edges
  • Mach Number
  • Mass Flow
  • Shape
  • Streamline Shape
  • Supersonic Flow
  • Supersonic Nozzles
  • Three Dimensional
  • Two Dimensional

Technology Areas

  • Hypersonics