Experimental and Calculated Characteristics of Three Wings of NACA 64-210 and 65-210 Airfoil Sections with and without 2 deg Washout

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1947
Accession Number
ADA801248

Entities

People

  • James C. Sivells

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Aircrafts
  • Airfoils
  • Airplanes
  • Aspect Ratio
  • Coefficients
  • Drag
  • Dynamic Pressure
  • Flow
  • Fluid Dynamics
  • Low Drag
  • Mach Number
  • Two Dimensional