New Developments in Computational Fluid Dynamics: Proceedings of the Sixth International Nobeyama Workshop on the New Century of Computational Fluid Dynamics, Nobeyama, Japan, April 21 to 24, 2003It is a joyful and ?tting moment that we, the friends, colleagues and suppo- ers of Prof. Kunio Kuwahara, dedicate this Workshop to Prof. Kuwahara. We gathered in late April of 2003 in the tranquility of Nobeyama mountain resorttocommemoratethe60thbirthdayofProf.Kuwaharawhichhadfallen in November, 2002. IntheculturalbackdropofEastAsia, the60thbirthdaycarriesadditional signi?cance. Looking back on the occasion of Kan-re-ki (the 60th birthday), a man is supposed to have accomplished something of meaningfulness and value. With these undertones, it will be a useful exerciseto recount the spl- did accomplishments of Prof. Kuwahara. The major professional achievements of Prof. Kuwahara may be c- pressed into two main categories. First and foremost, Prof. Kuwahara will long be recorded as the front-line pioneer in using numerical computations to tackle complex problems in ?uid mechanics. His unquenching zeal in com- tation and utilization of computers is unmatched throughout the globe. His infatuation with the Supercomputers of 1980's and 1990's is now a legend in the ?uid dynamics communities. He continues to stand tall on the leading edge of computational ?uid mechanics research and industrial applications. In short, Prof. Kuwahara has ?lled in a chapter in the history of modern ?uid dynamics research. |
Contents
I | 1 |
IV | 2 |
V | 3 |
VI | 4 |
VIII | 5 |
XI | 6 |
XII | 7 |
XIII | 9 |
LXXXIV | 126 |
LXXXVII | 127 |
LXXXIX | 128 |
XC | 130 |
XCII | 135 |
XCIII | 136 |
XCIV | 141 |
XCVII | 143 |
XIV | 11 |
XVI | 12 |
XVII | 15 |
XVIII | 19 |
XIX | 23 |
XX | 24 |
XXII | 27 |
XXIII | 31 |
XXV | 34 |
XXVI | 36 |
XXVII | 40 |
XXVIII | 44 |
XXIX | 47 |
XXXII | 48 |
XXXIII | 52 |
XXXIV | 53 |
XXXV | 54 |
XXXVI | 55 |
XXXVIII | 57 |
XXXIX | 60 |
XLII | 61 |
XLIV | 62 |
XLV | 64 |
XLVI | 66 |
XLVII | 68 |
XLVIII | 69 |
XLIX | 72 |
L | 73 |
LI | 74 |
LII | 77 |
LIII | 79 |
LIV | 81 |
LVII | 82 |
LVIII | 83 |
LIX | 86 |
LX | 89 |
LXI | 91 |
LXII | 92 |
LXV | 93 |
LXVI | 95 |
LXVII | 96 |
LXIX | 97 |
LXX | 101 |
LXXI | 102 |
LXXII | 103 |
LXXIII | 106 |
LXXIV | 109 |
LXXV | 112 |
LXXVI | 113 |
LXXVII | 114 |
LXXIX | 116 |
LXXX | 119 |
LXXXII | 122 |
LXXXIII | 125 |
XCVIII | 144 |
XCIX | 147 |
C | 152 |
CIII | 153 |
CIV | 154 |
CVI | 155 |
CVIII | 156 |
CIX | 158 |
CX | 162 |
CXI | 165 |
CXIV | 166 |
CXV | 167 |
CXVIII | 168 |
CXX | 169 |
CXXII | 172 |
CXXIII | 173 |
CXXIV | 175 |
CXXVII | 177 |
CXXVIII | 178 |
CXXIX | 179 |
CXXX | 180 |
CXXXI | 181 |
CXXXII | 183 |
CXXXIII | 186 |
CXXXVII | 187 |
CXXXIX | 188 |
CXL | 189 |
CXLII | 190 |
CXLIV | 191 |
CXLV | 192 |
CXLVII | 193 |
CXLVIII | 194 |
CXLIX | 195 |
CL | 196 |
CLI | 198 |
CLV | 200 |
CLVI | 202 |
CLVIII | 203 |
CLIX | 206 |
CLXIV | 207 |
CLXV | 209 |
CLXVII | 211 |
CLXVIII | 212 |
CLXIX | 213 |
CLXX | 215 |
CLXXI | 216 |
CLXXII | 217 |
CLXXIII | 220 |
CLXXIV | 222 |
CLXXV | 226 |
CLXXVI | 227 |
CLXXVII | 229 |
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accretion disc accuracy aerodynamic AIAA Paper airfoil algorithm amplitude analysis boundary conditions box-wing calculated Cartesian CCD scheme cells cluster 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 lift coefficient linear Mach number mode Nakahashi Navier-Stokes equations nodes Numerical Simulation obtained optimization parallel visualization system parameters performance physical Poisson equation pressure distributions problem Prof region Research 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 von Mises Stress vortices waveguides wing
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