Tests of a Double Wedge Aerofoil with a 30 per cent Control Flap over a Range of Supersonic Speeds

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Document Details

Document Type
Technical Report
Publication Date
Sep 08, 1945
Accession Number
ADA800690

Entities

People

  • F. W. Pruden

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Airfoils
  • Boundaries
  • Boundary Layer
  • Coefficients
  • Flaps (Control Surfaces)
  • Layers
  • Leading Edge Flaps
  • Leading Edges
  • Lepidoptera
  • Mach Number
  • Observation
  • Static Pressure
  • Trailing Edges
  • Translations
  • Two Dimensional
  • Waves
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow