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, 2003
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| Format: | Tagungsbericht Buch |
| Sprache: | English |
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Berlin [u.a.]
Springer
2005
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| Schriftenreihe: | Notes on numerical fluid mechanics and multidisciplinary design
90 |
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| Beschreibung: | Literaturangaben |
| Beschreibung: | 232 S. Ill., graph. Darst. 24 cm |
| ISBN: | 9783540274070 3540274073 |
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| 245 | 1 | 0 | |a New developments in computational fluid dynamics |b proceedings of the Sixth International Nobeyama Workshop on the New Century of Computational Fluid Dynamics, Nobeyama, Japan, April 21 to 24, 2003 |c Kozo Fujii ... (ed.) |
| 264 | 1 | |a Berlin [u.a.] |b Springer |c 2005 | |
| 300 | |a 232 S. |b Ill., graph. Darst. |c 24 cm | ||
| 336 | |b txt |2 rdacontent | ||
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| 490 | 1 | |a Notes on numerical fluid mechanics and multidisciplinary design |v 90 | |
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| 700 | 1 | |a Fujii, Kōzō |4 edt | |
| 711 | 2 | |a International Nobeyama Workshop on the New Century of Computational Fluid Dynamics |n 6 |d 2003 |c Nobeyama |j Sonstige |0 (DE-588)10122152-6 |4 oth | |
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Datensatz im Suchindex
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| adam_text | TABLE OF CONTENTS
A MULTIDOMAIN SPECTRAL COLLOCATION METHOD FOR COMPUTATIONAL
ELECTROMAGNETICS WITH APPLICATION TO OPTICAL WAVEGUIDES
..........
1
C.C. HUANG AND J.Y. YANG
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 1
2 FORMULATIONS OF WAVE EQUATIONS . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 2
3 NUMERICALTECHNIQUES ....................................... 3
3.1 MULTIDOMAIN SPECTRAL COLLOCATION METHOD . . . . . . . . . . . . . .
. . . 3
3.2 INTERFACIAL BOUNDARY CONDITIONS . . . . . . . . . . . . . . . . . .
. . . . . . . . 4
3.3 CARDINAL BASIS FUNCTIONS . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 4
4 DETERMINATION OF SCALING FACTOR . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . 5
5 NUMERICALRESULTSANDDISSCUSSION ............................ 5
5.1 FUNDAMENTAL MODE OF SYMMETRIC THREE-LAYER STEP-INDEX
WAVEGUIDES............................................ 5
5.2 ASYMMETRIC PLANAR WAVEGUIDE WITH EXPONENTIAL RIP . . . . . . . 6
5.3 SEMICONDUCTOR RIB WAVEGUIDE . . . . . . . . . . . . . . . . . . . .
. . . . . . . 7
6 CONCLUSION................................................. 9
THERMONUCLEAR SUPERNOVAE: COMBINING ASTROPHYSICAL AND
TERRESTRIAL COMBUSTION
.........................................
11
E. S. ORAN
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 11
2 THERMONUCLEARSUPERNOVAE................................... 12
3 TRANSITION FROM A DEFLAGRATION TO A DETONATION . . . . . . . . . . . .
. . . . . 15
4 CONCLUSIONSTODATE......................................... 19
HYPERSONIC MAGNETO-AERODYNAMIC INTERACTION
.....................
23
J. S. SHANG
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 23
2 EXPERIMENTAL FACILITY . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . 24
3 NUMERICAL SIMULATIONS . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . 24
4 NON-EQUILIBRIUM PHENOMENON . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 27
5 ELECTROMAGNETIC EFFECTS . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . 31
6 CONCLUSIONS ................................................ 31
SOME REMARKS ON THE CFD RESEARCH FOR SPACE TRANSPORTATION
SYSTEM DEVELOPMENT
...........................................
34
K. FUJII
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 34
1.1 RLV AERODYNAMICS * CFD CAPABILITY FOR THE ESTIMATION
OF RLV AERODYNAMICS- . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . 36
XII TABLE OF CONTENTS
1.2 SUPERSONIC BASE FLOWS -FINDING A NEW EFFICIENT TOOLS- . . . . . . 40
2 CONCLUSIONS ................................................ 44
DEVELOPMENT OF IMPLICIT LARGE EDDY SIMULATION
...................
47
K. KUWAHARA, S. KOMURASAKI, J. OOIDA, A. BETANCOURT
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 47
2 COMPUTATIONAL METHOD . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 48
3 COMPUTATIONAL RESULTS . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 52
3.1 REARRANGEMENTOFKARMANVORTEXSTREET .................. 52
3.2 TRANSITION TO TURBULENCE . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 53
3.3 TURBULENCE GENERATED BY A LATTICE . . . . . . . . . . . . . . . . .
. . . . . . 54
3.4 CIRCULAR CYLINDER . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 55
3.5 SUBSONIC FLOW AROUND AN AIRFOIL . . . . . . . . . . . . . . . . . .
. . . . . . . 55
3.6 SIMULATION WITH USING A BODY-FITTED GRID . . . . . . . . . . . . . .
. . . 57
DNA COMPUTING BASED ON ACTUAL BIOLOGICAL SEQUENCES AND
ACCURATE REACTION CONTROL
......................................
60
K. NAITOH
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 60
2 DNACOMPUTINGASNANO-COMPUTING ......................... 61
3 DNA COMPUTING USING ACTUAL LIVING ORGANISMS . . . . . . . . . . . . .
. . 61
3.1 PROBLEM SOLVED IN THIS SESSION . . . . . . . . . . . . . . . . . . .
. . . . . . . . 61
3.2 ENCODING BASED ON THE SEGMENTS OF BIOLOGICAL DNA CUT
BY RESTRICTION ENZYMES . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . 61
3.3 LIBRARY OF THE CANDIDATES OBTAINED WITH LIGATION
REACTIONS AND ANALYSIS OF THE ELECTROPHORESIS PHOTOGRAPHS . . 62
4 STRATEGY FOR CONTROLLING POLYMERASE
CHAIN REACTION (PCR) . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . 64
4.1 PCR.................................................. 64
4.2 CONTROL OF PCR FOR DNA COMPUTING . . . . . . . . . . . . . . . . . .
. . . 64
5 CONCLUSION................................................. 66
FROM ONE-MONTH CFD TO ONE-DAY CFD * EFFORTS FOR REDUCING
TIME AND COST OF CFD *
.......................................
68
K. NAKAHASHI, T. FUJITA AND Y. ITO
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 68
2 MESH GENERATION . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . 69
2.1 MESH GENERATION PROCEDURE . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . 69
2.2 SURFACE MESH GENERATION . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 69
3 PARALLEL FLOW SOLVER . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . 72
3.1 BASICFLOWSOLVER ...................................... 72
3.2 PARALLEL FLOW SOLVER . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . 73
4 NUMERICALEXAMPLES ........................................ 74
4.1 JAXA SUPERSONIC AIRPLANE IN ASCENDING FLIGHT . . . . . . . . . . . .
74
4.2 FLOWAROUNDA HORNET .................................. 77
TABLE OF CONTENTS XIII
5 SUMMARY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 79
NUMERICAL ATTEMPTS OF CAPTURING CONTACT SURFACE
.................
81
K. SAWADA, N. OHNISHI
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 81
2 NUMERICALMETHODS ......................................... 82
2.1 SCHEME-A (LAGRANGIAN BASED APPROACH) . . . . . . . . . . . . . . . .
. . 82
2.2 SCHEME-B(EULERIANBASEDAPPROACH)..................... 83
3 RESULTSANDDISCUSSIONS...................................... 86
4 CONCLUSIONS ................................................ 89
PARALLEL VISUALIZATION SYSTEMS
...................................
91
H. MIYACHI, S. HAYASHI, Y. NAKAI, Y. ITOH, M. SHIRAZAKI
AND R. HIMENO
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 91
2 VISUALIZATION PROCEDURE . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . 92
3 VARIOUS PARALLEL VISUALIZATION SYSTEMS . . . . . . . . . . . . . . . .
. . . . . . . . . 92
3.1 PARALLEL VOLUME RENDERING SYSTEM . . . . . . . . . . . . . . . . . .
. . . . . 92
3.2 ON-DEMAND PARALLEL RENDERING SYSTEM
[1]
................. 93
3.3 PARALLEL VISUALIZATION SYSTEM FOR CLUSTER MACHINE . . . . . . . . .
. 95
4 PERFORMANCE OF THE PARALLEL VISUALIZATION SYSTEMS . . . . . . . . . .
. . . . . 96
4.1 PERFORMANCE OF ON-DEMAND RENDERING SYSTEM . . . . . . . . . . . . .
96
4.2 PERFORMANCE OF PARALLEL VISUALIZATION SYSTEM
FORCLUSTERMACHINE .................................... 97
5 CONCLUSION................................................. 101
NUMERICAL SIMULATION OF TIME-DEPENDENT BUOYANCY-DRIVEN
CONVECTION IN AN ENCLOSURE
......................................
102
H.S. KWAK AND J.M. HYUN
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 102
2 ADVANCES IN NUMERICAL STUDIES . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . 103
3 RESONANT CONVECTION RESPONDING TO PERIODIC EXCITATIONS . . . . . . . .
106
4 CONCLUDINGREMARKS ........................................ 109
AUTOMATIC TOPOLOGY GENERATION
.................................
112
P.R. EISEMAN AND K. RAJAGOPALAN
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 112
2 GRIDPRO*S TOPOLOGICAL PARADIGM . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 113
3 CARTESIAN APPROACH TO AUTOMATIC TOPOLOGY GENERATION . . . . . . . . .
. 114
3.1 CARTESIAN TOPOLOGY GENERATION IN THREE DIMENSIONS . . . . . . . .
116
3.2 IMPROVEMENTS TO THE CARTESIAN TOPOLOGY GENERATION
TECHNIQUEIN3D........................................ 119
4 AUTOMATIC NESTED REFINEMENT . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . 119
5 APPLICATION OF NEST TO A THIN CURVED
WAVYTUBEINA BOX ........................................ 122
XIV TABLE OF CONTENTS
COMPUTATIONAL STUDY OF INFLUENCES OF A SEAM LINE
OF A BASEBALL ON FLOWS
..........................................
125
R. HIMENO
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 125
2 COMPUTATION METHOD . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 126
2.1 BASIC EQUATIONS . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 126
2.2 MACBASEDSCHEME .................................... 126
2.3 THIRD-ORDER UPWIND-DIFFERENCE SCHEME . . . . . . . . . . . . . . . .
. . . 127
3 GRIDSYSTEM................................................ 127
4 SHAPEOFTHESEAMONTHEBALL................................ 128
5 COMPUTEDRESULTS .......................................... 130
5.1 FOUR-SEAM CASE . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 130
5.2 TWO-SEAM CASE . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 135
6 CONCLUSIONS ................................................ 136
VORTEX BREAKDOWN FLOWS IN CYLINDRICAL GEOMETRY
..................
141
R. IWATSU
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 141
2 NUMERICALMODEL ........................................... 143
3 RESULTS .................................................... 144
3.1 TOP RIGID-COVER (CASE A) . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . 144
3.2 TOP FREE-SLIP-CONDITION (CASE B) . . . . . . . . . . . . . . . . . .
. . . . . . 147
AERODYNAMIC AND STRUCTURAL ANALYSES
OF JOINED WINGS OF HALE AIRCRAFT
.................................
152
R. SIVAJI, S. MARISARLA, V. NARAYANAN, V. KALOYANOVA, U. GHIA
AND K. N. GHIA
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 152
2 AERODYNAMIC ANALYSIS . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 153
3 STRUCTURALANALYSIS.......................................... 154
3.1 1-D APPROXIMATION OF 3-D JOINED-WING STRUCTURE:
AERODYNAMICS-STRUCTURE COUPLING. . . . . . . . . . . . . . . . . . . . .
. . . 154
3.2 BOX-WINGMODEL....................................... 155
3.3 REINFORCED SHELL MODEL . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . 155
4 RESULTSANDDISCUSSION ...................................... 156
4.1 AERODYNAMIC ANALYSIS . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 156
4.2 STRUCTURALANALYSIS..................................... 158
5 CONCLUSION................................................. 162
NUMERICAL SIMULATION OF FORMATION AND MOVEMENT
OF VARIOUS SAND DUNES
..........................................
165
R. ZHANG, T. KAWAMURA AND M. KAN
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 165
2 NUMERICALMETHODS ......................................... 166
2.1 CALCULATION OF THE AIR FLOW . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 167
TABLE OF CONTENTS XV
2.2 ESTIMATION OF SAND TRANSFER . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . 167
2.3 DETERMINATION OF THE SHAPE OF THE SAND DUNES . . . . . . . . . . . .
. 167
3 RESULTSANDDISCUSSION ...................................... 168
3.1 BARCHAN DUNES . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 168
3.2 TRANSVERSE DUNES . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . 169
3.3 LINEAR DUNES . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 169
3.4 CHINESEWALL .......................................... 172
4 CONCLUDINGREMARKS ........................................ 173
EVOLUTIONARY MULTI-OBJECTIVE OPTIMIZATION AND VISUALIZATION
.......
175
S. OBAYASHI
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 175
2 EVOLUTIONARY MULTIOBJECTIVE OPTIMIZATION . . . . . . . . . . . . . . .
. . . . . . . 177
2.1 MOGAS............................................... 177
2.2 CFD EVALUATION . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 177
2.3 NEURALNETWORKANDSOM............................... 177
2.4 CLUSTERANALYSIS........................................ 178
3 FOUR-OBJECTIVE OPTIMIZATION FOR SUPERSONIC
WINGDESIGN ............................................... 179
3.1 FORMULATION OF OPTIMIZATION . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . 179
3.2 VISUALIZATION OF DESIGN TRADEOFFS: SOM OF TRADEOFFS . . . . . . . .
180
3.3 DATA MINING OF DESIGN SPACE: SOM OF DESIGN VARIABLES . . . . . 181
4 CONCLUDINGREMARKS ........................................ 183
THE FRAMEWORK OF A SYSTEM FOR RECOMMENDING COMPUTATIONAL
PARAMETER CHOICES
.............................................
186
S. SHIRAYAMA
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 186
2 PARAMETER RECOMMENDATION SYSTEM . . . . . . . . . . . . . . . . . . .
. . . . . . . . 187
2.1 PARAMETERSTUDY....................................... 187
2.2 PARAMETERMINING...................................... 188
2.3 FRAMEWORK OF THE RECOMMENDATION SYSTEM . . . . . . . . . . . . . . .
. 189
3 COMPONENTS OF THE PARAMETER
RECOMMENDATION SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . 189
3.1 PARAMETERSPACE ....................................... 190
3.2 SEARCH PROCEDURE . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . 190
3.3 OPTIMIZATION BY GA AND RULE EXTRACTION
BYSCHEMAANALYSIS .................................... 191
4 SYSTEM IMPLEMENTATION . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 192
5 FRAMEWORK VERIFICATION BY NUMERICAL EXPERIMENTS . . . . . . . . . . .
. . . 192
5.1 EXPERIMENTALSYSTEM1.................................. 193
5.2 NUMERICAL EXPERIMENTS USING SYSTEM 1 AND DISCUSSION . . . . . 194
5.3 EXPERIMENTALSYSTEM2.................................. 195
6 CONCLUSION................................................. 196
XVI TABLE OF CONTENTS
GAS FLOW IN CLOSE BINARY STAR SYSTEMS
............................
198
T. MATSUDA, K. OKA, I.. HACHISU, H.M.J. BOFFIN
1 ACCRETION DISCS . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . 198
1.1 NUMERICAL SIMULATIONS OF GAS FLOW IN A CLOSE BINARY SYSTEM 198
1.2 MODERN CALCULATION OF ACCRETION FLOW . . . . . . . . . . . . . . . .
. . . . 200
1.3 DISCOVERY OF SPIRAL SHOCKS BY OBSERVATION . . . . . . . . . . . . .
. . . . 202
2 FLOW ON A COMPANION SURFACE . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . 202
2.1 FLOW PATTERN . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . 202
2.2 DOPPLERMAP .......................................... 203
FLOW SIMULATION USING COMBINED COMPACT DIFFERENCE SCHEME
WITH SPECTRAL-LIKE RESOLUTION
....................................
206
TOMONORI NIHEI (CSE, NAGOYA UNIVERSITY), KATSUYA ISHII (ITC,
NAGOYA UNIVERSITY)
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 206
2 COMBINED COMPACT DIFFERENCE SCHEME . . . . . . . . . . . . . . . . . .
. . . . . . . 207
3 SIMULATION OF INCOMPRESSIBLE FLOWS . . . . . . . . . . . . . . . . . .
. . . . . . . . . . 209
3.1 THE POISSON EQUATION SOLVER FOR TWO-DIMENSIONAL PROBLEMS . 209
3.2 THE POISSON EQUATION SOLVER FOR THREE-DIMENSIONAL PROBLEMS 211
3.3 THREE-DIMENSIONAL INCOMPRESSIBLE LID-DRIVEN CAVITY FLOW . . . . .
212
4 CONCLUSIONS ................................................ 213
A NEW HIGH ORDER FINITE VOLUME METHOD
FOR THE EULER EQUATIONS ON UNSTRUCTURED GRIDS
....................
215
Z.J. WANG
1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . 215
2 BASICIDEAOFTHESPECTRALVOLUMEMETHOD ..................... 216
3 NUMERICALRESULTS .......................................... 217
3.1 ACCURACY STUDY WITH VORTEX EVOLUTION PROBLEM . . . . . . . . . . . .
217
3.2 SCATTERING OF PERIODIC ACOUSTIC SOURCE
FROM TWO CYLINDERS . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . 220
4 CONCLUSIONS ................................................ 222
PARTICIPANTS PHOTOGRAPH
........................................
226
PARTICIPANTS LIST
...............................................
227
THE SIXTH INTERNATIONAL NOBEYAMA WORKSHOP ON THE NEW CENTURY
OF COMPUTATIONAL FLUID DYNAMICS
................................
229
|
| any_adam_object | 1 |
| author2 | Fujii, Kōzō |
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| building | Verbundindex |
| bvnumber | BV035367144 |
| classification_rvk | UF 4000 |
| ctrlnum | (OCoLC)181461095 (DE-599)DNB975231685 |
| discipline | Maschinenbau / Maschinenwesen Physik |
| format | Conference Proceeding Book |
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| indexdate | 2024-07-09T21:32:15Z |
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| isbn | 9783540274070 3540274073 |
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| spelling | 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, 2003 Kozo Fujii ... (ed.) Berlin [u.a.] Springer 2005 232 S. Ill., graph. Darst. 24 cm txt rdacontent n rdamedia nc rdacarrier Notes on numerical fluid mechanics and multidisciplinary design 90 Literaturangaben Numerische Strömungssimulation (DE-588)4690080-9 gnd rswk-swf (DE-588)1071861417 Konferenzschrift 2003 Nobeyama gnd-content Numerische Strömungssimulation (DE-588)4690080-9 s DE-604 Fujii, Kōzō edt International Nobeyama Workshop on the New Century of Computational Fluid Dynamics 6 2003 Nobeyama Sonstige (DE-588)10122152-6 oth Notes on numerical fluid mechanics and multidisciplinary design 90 (DE-604)BV014762175 90 text/html http://deposit.dnb.de/cgi-bin/dokserv?id=2647378&prov=M&dok_var=1&dok_ext=htm Inhaltstext DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=017171087&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | 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, 2003 Notes on numerical fluid mechanics and multidisciplinary design Numerische Strömungssimulation (DE-588)4690080-9 gnd |
| subject_GND | (DE-588)4690080-9 (DE-588)1071861417 |
| title | 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, 2003 |
| title_auth | 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, 2003 |
| title_exact_search | 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, 2003 |
| title_full | 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, 2003 Kozo Fujii ... (ed.) |
| title_fullStr | 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, 2003 Kozo Fujii ... (ed.) |
| title_full_unstemmed | 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, 2003 Kozo Fujii ... (ed.) |
| title_short | New developments in computational fluid dynamics |
| title_sort | 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 2003 |
| title_sub | proceedings of the Sixth International Nobeyama Workshop on the New Century of Computational Fluid Dynamics, Nobeyama, Japan, April 21 to 24, 2003 |
| topic | Numerische Strömungssimulation (DE-588)4690080-9 gnd |
| topic_facet | Numerische Strömungssimulation Konferenzschrift 2003 Nobeyama |
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