THE TWO DIMENSIONAL INFLOW CONDITIONS FOR A SUPERSONIC COMPRESSOR WITH CURVED BLADES

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1956
Accession Number
AD0101949

Entities

People

  • Phillip Levine

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Axial Flow
  • Compressors
  • Continuity
  • Curvature
  • Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Geometry
  • Government Procurement
  • Governments
  • Leading Edges
  • Mach Number
  • Mass Flow
  • Steady Flow
  • Two Dimensional

Technology Areas

  • Hypersonics