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Titlebook: Recent Advances in Computational Fluid Dynamics; Proceedings of the U C. C. Chao,S. A. Orszag,W. Shyy Conference proceedings 1989 Springer-

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A Unified Pressure Correction Algorithm for Computing Complex Fluid Flows,elocity components on arbitrary coordinates, and second-order accurate discretization. A number of two- and three-dimensional flow problems including the effects of turbulence, combustion, and compressibility are presented to demonstrate the capability of the present algorithm.
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The Application of Multiple One-Dimensional Adaptive Grid Method, distortion and the accuracy of temperature distribution are improved. The method is further applied to a transonic Euler Row by TVD scheme. Some modifications are illustrated and the result is satisfactory.
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Conference proceedings 1989sic and applied science. The development of computational fluid dynamics (CFD) has opened new areas of research and has significantly supplemented information available from experimental measurements. Scientific computing is directly responsible for such recent developments as the secondary instabil
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Conference proceedings 1989ulence, three-dimensional full-aircraft flow analyses, and so on. We believe that CFD has already achieved a status in the tool-kit of fluid mechanicians equal to that of the classical scientific techniques of mathematical analysis and laboratory experiment.
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Supercomputing and the Finite Element Approximation of the Navier-Stokes Equations for Incompressibe methodology discussed here is then applied to the simulation of jets in a cavity, using a CRAY X-MP supercomputer. Various visualizations of the numerical results are presented, in order to show the vortex dynamics taking place in the cavity.
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An Improved Upwind Scheme for the Euler Equations,uity. Since upwind differencing is naturally dissipative, the stability and accuracy of the present algorithm is enhanced. Numerical results demonstrate that the present scheme is as accurate as the TVD scheme [1] and as efficient as other upwind scheme [2].
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