LIFT AND MOMENT COEFFICIENTS EXPANDED TO THE SEVENTH POWER OF FREQUENCY FOR OSCILLATING RECTANGULAR WINGS IN SUPERSONIC FLOW AND APPLIED TO A SPECIFIC FLUTTER PROBLEM

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1954
Accession Number
AD0029127

Entities

People

  • Charles E. Watkins
  • Herbert C. Nelson
  • Ruby A. Rainey

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aeronautical Laboratories
  • Air Force
  • Aspect Ratio
  • Boundary Value Problems
  • Coordinate Systems
  • Differential Equations
  • Equations
  • Flow
  • Integrals
  • Leading Edges
  • Mach Number
  • Supersonic Flow
  • Trailing Edges
  • Translations
  • Two Dimensional
  • Wing Tips

Technology Areas

  • Hypersonics