WIND TUNNEL TESTS OF THIN AIRFOILS OSCILLATING NEAR STALL. VOLUME II. DATA REPORT

Abstract

The report presents the actual computer data that resulted from the two-dimensional tests of thin airfoils oscillating near stall. An introduction provides a general background, and a set of tables forms an index to specific data. More than 200 pages of computer data are included.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1969
Accession Number
AD0684324

Entities

People

  • Jaan Liiva
  • Lewis Gray

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Army Aviation
  • Coefficients
  • Computers
  • Dynamic Pressure
  • Frequency
  • Fungi
  • Intellectual Property
  • Load Distribution
  • Mach Number
  • Oscillation
  • Plastic Explosives
  • Rdx
  • Three Dimensional
  • Two Dimensional
  • United States
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics