EXPERIMENTAL INVESTIGATION OF A TRANSONIC AXIAL-FLOW-COMPRESSOR ROTOR WITH DOUBLE-CIRCULAR-ARC AIRFOIL BLADE SECTIONS. 1. DESIGN, OVER-ALL PERFORMANCE, AND STALL CHARACTERISTICS

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 05, 1954
Accession Number
AD0028969

Entities

People

  • Francis C. Schwenk
  • George K. Serovy
  • George W. Lewis Jr.

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Anemometers
  • Axial Flow
  • Axial Flow Compressors
  • Boundary Layer
  • Compressor Rotors
  • Compressors
  • Computational Fluid Dynamics
  • Flow
  • Geometry
  • Government Procurement
  • Guide Vanes
  • Hot Wire
  • Hot Wire Anemometers
  • Inlet Guide Vanes
  • Mach Number
  • Measurement
  • Static Pressure