Hingeless Rotor Servo-Aeroelasticity.

Abstract

Contents: Coriolis coupled bending vibrations of hingeless helicopter rotor blades; Scale effects in the bending vibrations of helicopter rotor blades; The influence of pitch and twist on blade vibrations; The dynamics of blade pitch control; Open and closed loop stability of hingeless rotor helicopter air and ground resonance; Stability and control of hingeless rotor helicopter ground resonance; Optimizing the cyclic control response of helicopter rotors.

Document Details

Document Type
Technical Report
Publication Date
Jul 24, 1975
Accession Number
ADA013574

Entities

People

  • Maurice I. Young

Organizations

  • University of Delaware

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeroelasticity
  • Aircrafts
  • Airframes
  • Dynamics
  • Helicopter Rotors
  • Helicopters
  • Hingeless
  • Motion
  • Resonance
  • Rotary Wing Aircraft
  • Vehicles
  • Vibration

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Control Systems Engineering.