Effect of Leakage Past Aileron Nose on Aerodynamic Characteristics of Plain and Internally Balanced Ailerons on NACA 66(215)-216, a = 1.0 Airfoil

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1945
Accession Number
ADA801271

Entities

People

  • J. D. Bird

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aeronautics
  • Coefficients
  • Dynamic Pressure
  • Free Stream
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Static Pressure
  • Surfaces
  • Trailing Edges
  • Two Dimensional
  • Two Dimensional Flow
  • Wind Tunnel Tests
  • Wind Tunnels