Single-Degree -of-Freedom-Flutter Calculations for a Wing in Subsonic Potential Flow and Comparison with an Experiment

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1951
Accession Number
ADA382127

Entities

People

  • Harry L. Runyan

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Altitude
  • Aspect Ratio
  • Ball Bearings
  • Flow
  • Fluid Dynamics
  • Frequency
  • High Altitude
  • Incompressible Flow
  • Mach Number
  • Potential Flow
  • Resonant Frequency
  • Three Dimensional
  • Two Dimensional