High-Subsonic Performance Characteristics and Boundary-Layer Investigations of a 12 deg 10-Inch-Inlet-Diameter Conical Diffuser

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Document Details

Document Type
Technical Report
Publication Date
May 11, 1950
Accession Number
ADA801178

Entities

People

  • B. H. Little Jr.
  • Stafford W. Wilbur

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Boundary Layer
  • Computational Science
  • Curvature
  • Dynamic Pressure
  • Flow
  • Flow Rate
  • Geometry
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Reynolds Number
  • Stagnation Pressure
  • Static Pressure