UNSTEADY STALL OF AXIAL FLOW COMPRESSORS

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1963
Accession Number
AD0401467

Entities

People

  • W. G. Brady

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Actuators
  • Aeronautical Laboratories
  • Axial Flow
  • Axial Flow Compressors
  • Boundary Layer
  • Differential Equations
  • Equations
  • Free Stream
  • Jet Engines
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Transducers
  • Static Pressure
  • Steady Flow
  • Turbojet Engines
  • Wind Tunnels