Aeroelastic stability of full-span tiltrotor aircraft model in forward flight

Author:

LI Zhiquan,XIA Pinqi

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference21 articles.

1. Whirl flutter and rotor hub center’s motion image of tiltrotor aircraft;Li;Sci China Technol Sci,2014

2. Propeller-rotor whirl flutter: a state-of-the-art review;Reed;J Sound Vib,1966

3. Johnson W. Dynamics of tilting proprotor aircraft in cruise flight. Washington, D.C.: NASA; 1974. Report No.: NASA TN D-7677.

4. Parametric studies for tiltrotor aeroelastic stability in high-speed flight;Nixon;J Am Helicopter Soc,1992

5. Nixon MW. Aeroelastic response and stability of tiltrotors with elastically-coupled composite rotor blades[dissertation]. Maryland: University of Maryland; 1994. p. 80–115.

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