LOAD DISTRIBUTIONS ASSOCIATED WITH CONTROLS AT SUPERSONIC SPEEDS

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Document Details

Document Type
Technical Report
Publication Date
May 29, 1953
Accession Number
AD0011094

Entities

People

  • Douglas R. Lord
  • K. R. Czarnecki

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Boundary Layer
  • Control Surfaces
  • Delta Wings
  • Flaps (Control Surfaces)
  • Flow
  • High Pressure
  • Laminar Boundary Layer
  • Leading Edges
  • Load Distribution
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Three Dimensional
  • Trailing Edges
  • Turbulent Boundary Layer
  • Two Dimensional

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow