A STUDY OF THE END WALL BOUNDARY LAYER IN AN AXIAL COMPRESSOR BLADE ROW

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1955
Accession Number
AD0092632

Entities

People

  • David L. Richardson
  • Raymond W. Moore Jr.

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Compressor Blades
  • Cross Flow
  • Equations
  • Fluid Flow
  • Free Stream
  • Gas Turbines
  • Geometry
  • Integral Equations
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Shear Stresses
  • Stagnation Pressure
  • Static Pressure
  • Turbulent Boundary Layer