PRESSURE RECOVERY AND MASS-FLOW PERFORMANCE OF FOUR ANNULAR NOSE INLETS OPERATING IN MACH NUMBER REGION OF 3.1 AND REYNOLDS NUMBER RANGE OF APPROXIMATELY 0.45 X 106 TO 20 X 106

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Document Details

Document Type
Technical Report
Publication Date
Mar 26, 1954
Accession Number
AD0028729

Entities

People

  • Henry R. Hunczak

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Curvature
  • Diffusers
  • Flow
  • Flow Fields
  • Free Stream
  • Geometry
  • Laminar Boundary Layer
  • Layers
  • Mach Number
  • Mass Flow
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Stagnation Pressure
  • Static Pressure