INVESTIGATION OF A 10-STAGE SUBSONIC AXIAL-FLOW RESEARCH COMPRESSOR V-EFFECT OF REDUCING INLET-GUIDE-VANE TURNING ON OVER-ALL AND INLET-STAGE PERFORMANCE

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Document Details

Document Type
Technical Report
Publication Date
Mar 15, 1954
Accession Number
AD0028586

Entities

People

  • George K. Serovy
  • Ray E. Budinger

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Axial Flow
  • Axial Flow Compressors
  • Boundaries
  • Boundary Layer
  • Compressors
  • Diagrams
  • Experimental Data
  • Flow
  • Government Procurement
  • Guide Vanes
  • Inlet Guide Vanes
  • Instrumentation
  • Jet Engines
  • Mach Number
  • Measurement
  • Static Pressure