Helicopter vibration suppression using simple pendulum absorbers on the rotor blade

Materias

• Rotors (Helicopters)
• Stability of helicopters
• Structural design

Ediciones (1)

• Helicopter vibration suppression using simple pendulum absorbers on the rotor blade (1982)

  National Aeronautics and Space Administration, Scientific and Technical Information Branch · inglés

Más obras de G. Alvin Pierce

Introduction To Structural Dynamics And Aeroelasticity