A wake bending unsteady dynamic inflow model of tiltrotor in conversion flight of tiltrotor aircraft

Author:

Yue HaiLong,Xia PinQi

Publisher

Springer Science and Business Media LLC

Reference15 articles.

1. Nixon M W, Langston C W, et al. Aeroelastic stability of a soft- in-plane gimballed tiltrotor model in hover. In: 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Seattle, 2001

2. Potsdam M, Yeo H, Johnson W. Rotor airloads prediction using loose aerodynamic/structural coupling. In: 60th AHS Annual Forum. Baltimore, 2004

3. He C J. Finite-state dynamic wake interference modeling for rotorcraft simulation. In: 53rd AHS Annual Forum. Virginia, 1997

4. Bertin J J, Smith M L. Incompressible flow about wings of finite span, aerodynamics for engineers. 3rd ed. Prentice-Hall, Upper Saddle River, NJ, 1998: 261–336

5. Saffman P G. Vortex Force and Bound Vorticity, Vortex Dynamics. Cambridge: Cambridge University Press, 1992. 46–48

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