Modeling and simulation for tiltrotor airplane

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 27, Issue 4, 2006, Pages 584-587

  Yang, Xi Li ^a   Zhu, Ji Hong ^a   Huang, Xing Li ^a   Hu, Chun Hua ^a   Sun, Zeng Qi ^a  

^a TSINGHUA UNIVERSITY   (China)

Author keywords

Blade element analysts theory; Gimballed rotor; Momentum theory; Tiltrotor

Indexed keywords

COMPUTER SIMULATION; FLIGHT DYNAMICS; HELICOPTER ROTORS; MATHEMATICAL MODELS; WINGS;

BLADE ELEMENT ANALYSTS THEORIES; GIMBALLED ROTORS; MOMENTUM THEORIES; TILTROTOR AIRCRAFTS;

AIRCRAFT;

EID: 33846132875     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (6)

1. Carlson E B. Optimal tiltrotor aircraft operations during power failure[D]. University of Minnesota, 1999.
2. Keller J A. Analysis and control of the transient aeroelastic response of rotors during shipboard engagement and disengagement operations[D]. Department of Aerospace Engineering, Graduate School, Pennsylvania State University, 2001.
3. Leishman J G. Principles of helicopter aerodynamics[M]. Cambridge University Press, 2000.
4. Johnson W. Helicopter theory[M]. 1980.
5. Gao Z, Chen R L Helicopter aerodynamics[M]. Beijing: Press of Science, 2003. (in Chinese)
6. Li J B, Gao Z. Aerodynamic modeling and experiment for simulation of helicopter maneuver flight[J]. Acta Aeronautica et Astronautica Sinica, 2003, 24 (2): 116-118. (in Chinese)