Preliminary Investigation at Low Speeds of Swept Wings in Yawing Flow

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Document Details

Document Type
Technical Report
Publication Date
Feb 04, 1948
Accession Number
ADA800814

Entities

People

  • Alex Goodman
  • David Feigenbaum

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aircrafts
  • Aspect Ratio
  • Boundary Layer
  • Coefficients
  • Curvature
  • Flight
  • Flight Paths
  • High Lift
  • Layers
  • Leading Edges
  • Pressure Gradients
  • Static Pressure
  • Swept Wings
  • Sweptback Wings
  • Sweptforward Wings