Considerations of the Total Drag of Supersonic Airfoil Sections

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1947
Accession Number
ADB805337

Entities

People

  • E. B. Klunker
  • H. R. Ivey

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautics
  • Boundary Layer
  • Drag
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Laminar Boundary Layer
  • Layers
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Shape
  • Shock Waves
  • Supersonic Airfoils
  • Turbulent Flow

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight