Flight Dynamics Modeling, Trim, Stability, and Controllability of Coaxial Compound Helicopters

Author:

Cao Yihua1,Wang Maosheng2ORCID,Li Guozhi3

Affiliation:

1. Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, People’s Republic of China.

2. Master, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, People’s Republic of China (corresponding author). ORCID: .

3. School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, People’s Republic of China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference17 articles.

1. Cheney M. C. 1969. “The ABC helicopter.” In Proc. VTOL Research Design and Operations Meeting. Reston VA: American Institute of Aeronautics and Astronautics.

2. Coleman C. P. 1997. A survey of theoretical and experimental coaxial rotor aerodynamic research. Rep. No. NASA TP3675. Washington DC: National Aeronautics and Space Administration.

3. Aerodynamic characteristics of rigid coaxial rotor by wind tunnel test and numerical calculation

4. Fegely C. O. Juhasz H. Xin and M. B. Tischler. 2016. “Flight dynamics and control modeling with system identification validation of the Sikorsky X2 technology demonstrator.” In Proc. AHS Int. 72nd Annual Forum. West Palm Beach FL: American Helicopter Society.

5. Feil R. J. Rauleder and M. Hajek. 2016. “Aeromechanics analysis of a coaxial rotor system in hover and high-advance-ratio forward flight.” In Proc. 34th AIAA Applied Aerodynamics Conf. Washington DC: American Institute of Aeronautics and Astronautics.

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