SOME EFFECTS OF FLOW SEPARATION ON THE OVERALL FORCE CHARACTERISTICS OF THIN WINGS OF ASPECT RATIO 2 TO 4

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1955
Accession Number
AD0091753

Entities

People

  • A. L. Courtney

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircrafts
  • Aspect Ratio
  • Delta Wings
  • Flow Separation
  • Free Stream
  • High Lift
  • Leading Edges
  • Mach Number
  • Reynolds Number
  • Spars
  • Swept Wings
  • Sweptback Wings
  • Thin Wings
  • Two Dimensional
  • Wind Tunnels