Helicopter Blade Flutter

Abstract

Methods of analysis of helicopter blade flutter for both hinged and hingeless blades are presented. The major types considered are bending-torsion flutter, flap-lag flutter, and stall flutter. Both hover and forward flight are considered. Means of avoiding flutter are described.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1973
Accession Number
AD0756726

Entities

People

  • Norman D. Ham

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Loading
  • Aeroelasticity
  • Aircrafts
  • Control Systems
  • Equations
  • Equations Of Motion
  • Frequency
  • Geometry
  • Helicopter Rotors
  • Helicopters
  • Leading Edges
  • Nato
  • Pressure Distribution
  • Steady State
  • Two Dimensional
  • United States
  • Vibration

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerospace Engineering
  • Systems Analysis and Design