Tuft Studies of the Flow over a Wing at Four Angles of Sweep

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Document Details

Document Type
Technical Report
Publication Date
Jul 10, 1947
Accession Number
ADA800921

Entities

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Boundaries
  • Boundary Layer
  • Flow
  • Free Stream
  • Leading Edges
  • Mach Number
  • Military Organizations
  • Photographs
  • Pressure Distribution
  • Pressure Gradients
  • Swept Wings
  • Trailing Edges
  • Unsteady Flow