GENERAL CONSIDERATIONS OF MACH NUMBER EFFECTS ON COMPRESSOR-BLADE DESIGN

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Document Details

Document Type
Technical Report
Publication Date
Apr 07, 1954
Accession Number
AD0028872

Entities

People

  • John F. Klapproth

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Air Flow
  • Boundary Layer
  • Compressor Blades
  • Compressors
  • Equations
  • Flow
  • Flow Separation
  • Government Procurement
  • Guide Vanes
  • Inlet Guide Vanes
  • Leading Edges
  • Mach Number
  • Mass Flow
  • Stagnation Pressure
  • Static Pressure
  • Supersonic Flow
  • Surfaces