Boundary-Layer Measurements in 3.84- by 10-Inch Supersonic Channel

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1950
Accession Number
ADA382107

Entities

People

  • Paul F. Brinich

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Boundary Layer
  • Boundary Layer Flow
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Heat Transfer
  • Mach Number
  • Measurement
  • Prandtl Number
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Reynolds Number
  • Skin Friction
  • Static Pressure
  • Three Dimensional
  • Turbulent Boundary Layer

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow