Performance of an Axial-Flow Compressor Rotor Designed for a Pitch-Section Lift Coefficient of 1.20

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1947
Accession Number
ADA800820

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 Compressors
  • Coefficients
  • Compressor Blades
  • Compressor Rotors
  • Compressors
  • Efficiency
  • Flow
  • High Pressure
  • Leading Edges
  • Rotors
  • Roughness
  • Static Pressure
  • Surface Properties