PRELIMINARY MEASUREMENTS OF NONSTEADY VELOCITIES IN A SINGLE STAGE AXIAL-FLOW COMPRESSOR

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1956
Accession Number
AD0102522

Entities

People

  • Donald E. Andrews
  • Harry M. Croner
  • Hsuan Yeh

Organizations

  • Johns Hopkins University

Tags

DTIC Thesaurus Topics

  • Air Force
  • Axial Flow
  • Axial Flow Compressors
  • Boundary Layer
  • Compressors
  • Dynamic Pressure
  • Flow
  • Fluid Dynamics
  • Guide Vanes
  • Hot Wire
  • Hot Wire Anemometers
  • Inlet Guide Vanes
  • Intensity
  • Measurement
  • Pressure Distribution
  • Trailing Edges
  • Turbulence