Unconditional stable solutions of the Euler equations for two-and three-d wings in arbitrary motion

Author:

Zhenghong Gao

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference6 articles.

1. H. W. M. Hoeijmakers, et al., Numerical simulation of vortical flow over a delta wing at subsonic and transonic speed,Proceedings of the 17th ICAS Congress in 1990 ICAS-90-3.3.3 (1990).

2. A. Jameson, et al., Numerical Solution of Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Scheme,AIAA paper 81-1259 (1981).

3. D. L. Wtitefiled and J. M. Janus, Three-Dimensional Unsteady Euler Equations Solution Using Flux Vector Splitting,AIAA paper 84-1014 (1984).

4. H. Hollanders, et al., Three-Dimensional calculation of transonic viscous flows by an implicity method,AIAA J.,23, 11 (1985), 1670–1678.

5. P. C. E. Jorgenson, et al., An unconditional stable Runge-Kutta method for unsteady flows,27th Aerospace Sciences Meeting, Reno, Nevade, Jan. 9–12 (1989).

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