An Aerodynamic Design Method for Transonic Axial Flow Compressor Stage,

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Document Details

Document Type
Technical Report
Publication Date
Jul 21, 1982
Accession Number
ADA118278

Entities

People

  • Fang-yuan Zhu
  • Xin-hai Zhou

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Airfoils
  • Axial Flow
  • Axial Flow Compressors
  • Blades
  • Compressors
  • Computational Science
  • Computer Programs
  • Computers
  • Equations
  • Flow
  • Flow Fields
  • Foreign Technology
  • Free Stream
  • Leading Edges
  • Mach Number
  • Three Dimensional
  • Trailing Edges