A Method for Calculating Three-Dimensional Flow in Bladed Turbomachines by Using Arbitrary Quasi Perpendicular Intersecting Planes,

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Document Details

Document Type
Technical Report
Publication Date
Oct 09, 1981
Accession Number
ADA106475

Entities

People

  • Jiang Jinliang
  • Xin Xiaokang

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axial Flow
  • Centrifugal Compressors
  • Compressors
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Differential Equations
  • Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Fluid Flow
  • Foreign Technology
  • Internal Combustion Engines
  • Mach Number
  • Three Dimensional
  • Three Dimensional Flow