@article{(Open Science Index):https://publications.waset.org/pdf/6578,
	  title     = {Numerical Investigation of a Slender Delta Wing in Combined Force-Pitch and Free-Roll},
	  author    = {Yang Xiaoliang and  Liu Wei and  Wang Hongbo and  Zhao Yunfei},
	  country	= {},
	  institution	= {},
	  abstract     = {Numerical investigation of the characteristics of an 80°
delta wing in combined force-pitch and free-roll is presented. The
implicit, upwind, flux-difference splitting, finite volume scheme and
the second-order-accurate finite difference scheme are employed to
solve the flow governing equations and Euler rigid-body dynamics
equations, respectively. The characteristics of the delta wing in
combined free-roll and large amplitude force-pitch is obtained
numerically and shows a well agreement with experimental data
qualitatively. The motion in combined force-pitch and free-roll
significantly reduces the lift force and transverse stabilities of the delta
wing, which is closely related to the flying safety. Investigations on
sensitive factors indicate that the roll-axis moment of inertia and the
structural damping have great influence on the frequency and
amplitude, respectively. Moreover, the turbulence model is considered
as an influencing factor in the investigation.},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {5},
	  number    = {7},
	  year      = {2011},
	  pages     = {1482 - 1488},
	  ee        = {https://publications.waset.org/pdf/6578},
	  url   	= {https://publications.waset.org/vol/55},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 55, 2011},
	}