Effects of Modifications to the Leading-Edge Region on the Stalling Characteristics of the NACA 63(sub 1)-012 Airfoil Section

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1950
Accession Number
ADA382217

Entities

People

  • John A. Kelly

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Airfoils
  • Boundary Layer
  • Dynamic Pressure
  • Flow
  • Flow Separation
  • Laminar Boundary Layer
  • Layers
  • Leading Edge Flaps
  • Leading Edges
  • Pressure Distribution
  • Pressure Gradients
  • Static Pressure
  • Surfaces
  • Thickness
  • Trailing Edges
  • Turbulent Flow