[1] Borland, C., D. Rizzetta and H. Yoshihara, Numerical solution of three-dimensional unsteady transonic flow over swept wings, AIAA-paper 80-1369, July(1980).
[2] Sankar, L. N., J. B. Malone and Y. Tassa., An implicit conservative algorithm for steady and unsteady three-dimensional transonic potential flows, Proceedings of the AIAA Fifth Computational Fluid Dynamics Conference, Palo Alto, CA, June(1981), 199-212.
[3] Jameson, A. and V. Venkatakrishnan, Transonic flow about oscillating airfoils using the Euler equations, AIAA-paper 85-1514(1985).
[4] Chyu, W. J., S. S. Davis and K. S. Chang, Calculation of unsteady transonic flow over an airfoil, AIAA Journal, 19, 6(1981), 684-690.
[5] Gao, Z. H., Steady and unsteady transonic flow using the Euler equations, Ph. D. Thesis in Northwestern Polytechnical University (1989).
[6] Thomas, J. L., B. Van Leer and R. W. Walfer, Implicit flux-split schemes for the Euler equations, AIAA-paper 85-1680(1985).
[7] Thompson, J. F., Grid generation techniques on computational fluid dynamics, AIAA Journal, 22(1984), 1505.
[8] Gao, Z. H., The time-dependent body fitted Corrrkinate generation with the multigrid method, Acta Aeronautica et Astronautica Sinica, 9, 3(1988).(in Chinese)
[9] Gao, Z. H. and Liu, Q. G., A kind of improved flux-split method for solving the Euler equatins.(to be published.)
[10] Davis, S. S. and G. N. Malcolm, Experimental unsteady aerodynamics of conventional and super-critical airfoils, NACA TM 81221.
[11] Davis, S. S. and G. N. Malcolm, Experiments in unsteady transonic flow, Proceedings of AIAA/ASME/AHS 20th Structures, Structural Dynamics and Matericals Conference, St.Loris, Mo., April(1979). |
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