Boundary-Layer-Control Test of Two Wings in the Langley Propeller-Research Tunnel

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1946
Accession Number
ADA801294

Entities

People

  • Hugh B. Freeman

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aeronautics
  • Airfoils
  • Aspect Ratio
  • Boundaries
  • Boundary Layer
  • Boundary Layer Control
  • Dynamic Pressure
  • Free Stream
  • High Angles
  • High Lift
  • Leading Edges
  • Static Pressure
  • Suction Slots
  • Thick Wings
  • Thin Wings