Study on the dynamics of a rotor in a maneuvering aircraft

Journal of Vibration and Acoustics, Transactions of the ASME

Volumn 125, Issue 3, 2003, Pages 324-327

  Lin, Fusheng ^a   Meng, Guang ^a  

^a SHANGHAI JIAO TONG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; GRAVITATIONAL EFFECTS; ROTORS;

FLIGHT PATH INCLINATION;

FLIGHT DYNAMICS;

EID: 0038036245     PISSN: 10489002     EISSN: 15288927     Source Type: Journal    
DOI: 10.1115/1.1576422     Document Type: Article

References (7)

1. Lee, A. C., Kang, Y., Tsai, K. L., and Hsiao, K. M., 1992, “Transient Analysis of an Asymmetric Rotor-Bearing System during Acceleration,” ASME J. Ind., 114(4), pp. 465-475.
2. Ganesan, R., and Sankar, T. S., 1993, “Resonant Oscillations and Stability of Asymmetric Rotors,” Proc. of the 14th Biennial ASME Conference on Mechanical Vibration and Noise, ASME DE, 56, pp. 19-22.
3. Spence, A. M., and Cele, R., 1995, “Coupled Rotor Fuselage Dynamics and Aero-Elasticity in Turning Flight,” J. Am. Helicopter Soc., 40(1), pp. 47-58.
4. Cao, Y., 1999, “Modelling the Unsteady Aerodynamic Forces of a Maneuvering Rotor,” Aircraft Engineering and Aerospace Technol., 71(5), pp. 444-450.
5. Bagai, A., Leishman, J. G., and Park, J., 1999, “Aerodynamic Analysis of a Helicopter in Steady Maneuvering Flight Using a Free-Vortex Rotor Wake Model,” J. Am. Helicopter Soc., 44(2), pp. 109-120.
6. Park, J. S., and Leishman, J. G., 1999, “Investigation of Unsteady Aerodynamics on Rotor Wake Effects in Maneuvering Flight,” Annual Forum Proceedings-American Helicopter Society, 1, pp. 467-480.
7. Krothapalli, K. R., Prasad, J. V. R., and Peters, D. A., 2001, “Helicopter Rotor Dynamic Inflow Modelling for Maneuvering Flight,” J. Am. Helicopter Soc., 46(2), pp. 129-139.