 |
|
What people are saying - Write a reviewNew Developments in Computational Fluid Dynamics-Academic exchangesEditorial Review - 5zu.cnTitle: New Developments in Computational Fluid Dynamics: Proceedings of the Sixth International Nobeyama Workshop on the New Century of Computational Fluid ... Read full review Contents
Common terms and phrasesaccretion disc accuracy aerodynamic AIAA Paper airfoil algorithm analysis boundary conditions box-wing calculated Cartesian CCD scheme cells cluster collocation method Computational Fluid Dynamics computed results configuration contact surface contours convection degrees density design variables detonation DNA computer domain drag Engineering experimental Figure finite finite volume method flame flow field flow simulations flux geometry grid points grid system GridPro Hyun interaction interface Japan Kuwahara LES/RANS hybrid method lift coefficient Mach number Nakahashi Navier-Stokes equations nodes Numerical Simulation obtained optimization parallel visualization system parameters performance physical Poisson equation pressure distributions problem Prof region Research resonance Reynolds number Richtmyer-Meshkov instability rotation sand dunes Scheme-B seam shape Shell Model shock wave shown in Fig shows solution solved space star structure supersonic SV scheme temperature thermal three-dimensional tion Tohoku University topology turbulence model unsteady unstructured grids upwind scheme vector velocity viscous Volume vortex vortices waveguides wing Popular passagesPage iii - Zorneding Germany E-mail: ehhirschel@t-online.de Prof. Dr. Kozo Fujii Space Transportation Research Division The Institute of Space and Astronautical Science 3-1-1, Yoshinodai, Sagamihara, Kanagawa, 229-8510 Japan E-mail: fujii@flab.eng.isas.ac.jp Dr. Page iii - Prof. Dr. Bram van Leer Department of Aerospace Engineering The University of Michigan Ann Arbor, MI 48109-2140 USA Prof. Page 57 - Computation of high Reynolds number flow around a circular cylinder with surface roughness" , AIAA paper, 84-0340 Miyata, T. Page viii - Numerical Studies of Two-Dimensional Vortex Motion by a System of Point Vortices'. Page 196 - Department of Earth Science and Astronomy, College of Arts and Sciences, University of Tokyo, Komaba, Meguro-ku, Tokyo 153, Japan Recently, several "tree... Page 176 - ... of the winner unit. This process is repeated a number of times. In one training step, one sample vector is drawn randomly from the input data set. This vector is fed to all units in the network and a similarity measure is calculated between the input data sample and all the codebook vectors. The bestmatching unit is chosen to be the codebook vector with greatest similarity with the input sample. The similarity is usually defined by means of a distance measure. For example in the case of Euclidean... Page 88 - S., Numerical experiments with the Osher upwind scheme for the Euler equations, AIAA/ ASME; June 11. Page 7 - This research was financially supported by the National Science Council, Taiwan, Republic of China under contract No. Page 44 - ... Fin of the X- 1 5 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0," NASA TN D-6348, May 1971. Coin, KL, "Effect of Planform, Airfoil Section, and Angle-of-Attack on the Pressures Along the Base of Blunt-Trailing-Edge Wings at Mach Numbers of 1.41, 1.62, and 1.96," NACA RM L52D21, 1952. Herrin, JL, and Dutton, JC, "Supersonic Base Flow Experiments in the Near Wake of a Cylindrical Afterbody," AIAA Journal, January 1994, pp. Page 8 - Propagation characteristics of optical waveguiding structures by direct solution of the Helmholtz equation for total fields", J. References from web pagesNew Developments in Computational Fluid Dynamics - FORUM akademi GSCI Digest Donnerstag, Dezember 22, 2005 Volume 2006: Issue 01 ... 5525-Covers 1&4-standard.indd Bibliographic information |
