Two-Dimensional Wind-Tunnel Investigation of a 10.7-Percent-Thick Symmetrical Tail Section with a 0.40 Airfoil-Chord Control Surface and a 0.20 Control-Surface-Chord Tab

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1947
Accession Number
ADA801124

Entities

People

  • Albert L. Braslow

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Air Flow
  • Boundary Layer
  • Control Surfaces
  • Deflection
  • Flow
  • Fluid Dynamics
  • Free Stream
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Shape
  • Trailing Edges
  • Two Dimensional
  • Wind Tunnels