Performance of Axial-Flow Fan and Compressor Blades Designed for High Loadings

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1947
Accession Number
ADA800905

Entities

People

  • L. J. Herrig
  • Seymour M. Bogdonoff

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Axial Flow
  • Axial Flow Fans
  • Blowers
  • Coefficients
  • Compressor Blades
  • Compressors
  • Dynamic Pressure
  • Efficiency
  • Fans
  • Flow
  • Leading Edges
  • Pressure Distribution
  • Roughness
  • Static Pressure
  • Two Dimensional