EXPERIMENTAL INVESTIGATION OF ROTATING STALL AND BLADE VIBRATION IN THE AXIAL-FLOW COMPRESSOR OF A TURBOJET ENGINE

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1954
Accession Number
AD0029121

Entities

People

  • Andre J. Meyer
  • Howard F. Calvert
  • Merle C. Huppert

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Anemometers
  • Axial Flow
  • Axial Flow Compressors
  • Compressor Blades
  • Compressors
  • Engines
  • Frequency
  • Government Procurement
  • Guide Vanes
  • Hot Wire
  • Hot Wire Anemometers
  • Measurement
  • Production
  • Static Tests
  • Strain Gages
  • Turbojet Engines
  • Vibration