Interactional Aerodynamics of the Single Rotor Helicopter Configuration. Volume V. Harmonic Analyses of Hub Wake.

Abstract

Volume V of this series contains computer print-outs displaying the results of harmonic analyses of selected test runs. The steady and 10-harmonic coefficients for wake flow angles and associated velocity components are shown. This material is compiled to enable understanding of the wake structure additional to that derived from the spectrographs in other volumes. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1978
Accession Number
ADA063245

Entities

People

  • Philip F. Sheridan

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamics
  • Air Ejectors
  • Air Pressure
  • Aircrafts
  • Airframes
  • Anti-Radiation Missiles
  • Computer Programs
  • Flow
  • Frequency
  • Geometry
  • Harmonic Analysis
  • Helicopters
  • Insensitive Explosives
  • Materials
  • Phase
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
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