Modern computational aeroelasticity
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| LEADER | 00000nam a2200000 c 4500 | ||
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| 001 | BV047282426 | ||
| 003 | DE-604 | ||
| 005 | 20210601 | ||
| 007 | t| | ||
| 008 | 210512s2021 gw a||| |||| 00||| eng d | ||
| 015 | |a 17,N41 |2 dnb | ||
| 015 | |a 21,A06 |2 dnb | ||
| 016 | 7 | |a 1140858076 |2 DE-101 | |
| 020 | |a 9783110576474 |c Festeinband : EUR 120.95 (DE) (freier Preis), EUR 122.00 (AT) (freier Preis) |9 978-3-11-057647-4 | ||
| 020 | |a 3110576473 |9 3-11-057647-3 | ||
| 024 | 3 | |a 9783110576474 | |
| 035 | |a (OCoLC)1237113833 | ||
| 035 | |a (DE-599)DNB1140858076 | ||
| 040 | |a DE-604 |b ger |e rda | ||
| 041 | 0 | |a eng | |
| 044 | |a gw |c XA-DE-BE | ||
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| 084 | |8 3\p |a 510 |2 23sdnb | ||
| 084 | |8 1\p |a 620 |2 23sdnb | ||
| 100 | 1 | |a Xu, Min |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Modern computational aeroelasticity |c Min Xu, Xiaomin An, Wei Kang, Guangning Li |
| 264 | 1 | |a Berlin |b De Gruyter |c [2021] | |
| 300 | |a XI, 315 Seiten |b Illustrationen, Diagramme | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 650 | 0 | 7 | |a Aeroelastizität |0 (DE-588)4202469-9 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Numerisches Verfahren |0 (DE-588)4128130-5 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Aeroelastizität |0 (DE-588)4202469-9 |D s |
| 689 | 0 | 1 | |a Numerisches Verfahren |0 (DE-588)4128130-5 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a An, Xiaomin |e Verfasser |4 aut | |
| 700 | 1 | |a Kang, Wei |e Verfasser |4 aut | |
| 700 | 1 | |a Li, Guangning |e Verfasser |4 aut | |
| 710 | 2 | |a Walter de Gruyter GmbH & Co. KG |0 (DE-588)10095502-2 |4 pbl | |
| 776 | 0 | 8 | |i Erscheint auch als |n Online-Ausgabe |z 978-3-11-057668-9 |
| 776 | 0 | 8 | |i Erscheint auch als |n Online-Ausgabe, EPUB |z 978-3-11-057662-7 |
| 856 | 4 | 2 | |m X:MVB |u http://www.degruyter.com/search?f_0=isbnissn&q_0=9783110576474&searchTitles=true |
| 856 | 4 | 2 | |m B:DE-101 |q application/pdf |u https://d-nb.info/1140858076/04 |3 Inhaltsverzeichnis |
| 856 | 4 | 2 | |m DNB Datenaustausch |q application/pdf |u http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=032685937&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |3 Inhaltsverzeichnis |
| 883 | 2 | |8 1\p |a dnb |d 20210201 |q DE-101 |u https://d-nb.info/provenance/plan#dnb | |
| 883 | 2 | |8 2\p |a dnb |d 20210201 |q DE-101 |u https://d-nb.info/provenance/plan#dnb | |
| 883 | 2 | |8 3\p |a dnb |d 20210201 |q DE-101 |u https://d-nb.info/provenance/plan#dnb | |
| 943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-032685937 | |
Datensatz im Suchindex
| _version_ | 1819667884287197184 |
|---|---|
| adam_text | CONTENTS
PREFACE
*
V
CHAPTER
1
INTRODUCTION
*
1
1.1
1.2
1.3
1.4
DEVELOPMENT
HISTORY
OF
AEROELASTICITY
*
2
COMPUTATIONAL
AEROELASTICITY
METHOD
*
4
COMPUTATIONAL
AEROELASTICITY
SOFTWARE
*
7
KEY
TECHNIQUES
FOR
SOLVING
AEROELASTIC
PROBLEMS
BY
CFD/CSD
COUPLING
METHOD
*
8
1.4.1
SIMULATION
OF
NONLINEAR
CHARACTERISTICS
OF
THE
FLUID
AND
SOLID
DOMAINS
*
9
1.4.2
1.4.3
MOTION
STRATEGY
FOR
MOVING
GRID
*
9
CONTINUITY
AND
COMPATIBILITY
CONDITIONS
FOR
FLUID
AND
STRUCTURE
INTERFACE
*
9
1.4.4
CALCULATION
EFFICIENCY
OF
FLUID
AND
STRUCTURE
COUPLING
*
10
BIBLIOGRAPHY
-----
11
CHAPTER
2
UNSTEADY
CFD
TECHNOLOGY
*
13
2.1
2.2
2.3
2.4
2.4.1
2.4.2
2.4.3
2.4.4
2.5
INTRODUCTION
*
13
GOVERNING
EQUATIONS
*
13
FINITE
VOLUME
METHOD
*
15
SPATIAL
DISCRETIZATION
METHODOLOGIES
*
17
CENTRAL
SCHEME
WITH
ARTIFICIAL
DISSIPATION
*
19
VAN
LEER
*
S
FVS
SCHEME
*
21
ROE
*
S
FDS
SCHEME
-----
22
AUSM
SCHEME
-----
23
LIMITER
FUNCTIONS
AND
MONOTONE
UPSTREAM-CENTERED
SCHEME
FOR
CONSERVATION
LAWS
INTERPOLATION
*
26
2.6
2.6.1
2.6.2
2.6.3
2.7
2.7.1
2.7.2
2.7.3
2.7.4
2.8
2.9
TEMPORAL
DISCRETIZATION
*
29
EXPLICIT
TIME-ADVANCING
SCHEMES
*
30
IMPLICIT
TIME-ADVANCING
SCHEMES
*
30
SECOND-ORDER
IMPLICIT
TIME-ADVANCING
SCHEMES
*
34
TURBULENCE
MODELING
*
35
BALDWIN-LOMAX
ALGEBRAIC
MODEL
*
36
SPALART-ALLMARAS
ONE-EQUATION
MODEL
*
37
K-(I)
SST
TWO-EQUATION
MODEL
-----
39
DETACHED
EDDY
SIMULATION
*
40
GEOMETRIC
CONSERVATION
LAW
*
42
EXAMPLES
OF
CFD
IN
ENGINEERING
*
42
VIII
*
CONTENTS
2.9.1
TWO-DIMENSIONAL
AIRFOIL
OF
RAE2822-----
43
2.9.2
WING/BODY/TAIL
CONFIGURATION
OF
NASA
CRM-----
44
2.9.3
WING/BODY/PYLON/NACELLE
CONFIGURATION
OF
DLR-F6
-----
45
2.9.4
UNSTEADY
COMPUTATION
OF
AGARD
CT-5
-----
49
BIBLIOGRAPHY
-----
53
CHAPTER
3
NUMERICAL
METHOD
FOR
NONLINEAR
STRUCTURAL
RESPONSE
COMPUTATION
WITH
GEOMETRIC
NONLINEARITY
*
57
3.1
INTRODUCTION
*
57
3.2
DEFORMATION
AND
MOVEMENT
*
59
3.2.1
DEFINITION
OF
VARIABLES
AND
COORDINATE
SYSTEM
*
59
3.2.2
STRAIN
MEASUREMENT
*
64
3.2.3
STRESS
MEASUREMENT
*
66
3.2.4
LAGRANGIAN
CONSERVATION
EQUATION
*
67
3.3
VARIATIONAL
PRINCIPLE
*
69
3.3.1
CLASSICAL
VARIATIONAL
PRINCIPLE
OF
ELASTICITY
THEORY
*
69
3.3.2
GENERALIZED
VARIATIONAL
PRINCIPLE
OF
ELASTICITY
THEORY
*
73
3.4
MULTIVARIATE
SOLID-SHELL
ELEMENT
*
79
3.4.1
THREE
FIELDS
FRAEIJS
DE
VEUBEKE-HU-WASHIZU
VARIATIONAL
PRINCIPLE
*
79
3.4.2
NONLINEAR
FINITE
ELEMENT
DISCRETIZATION
*
80
3.4.3
PROCEDURE
OF
SOLVING
ALGORITHM
*
80
3.3.4
RESULTS
AND
ANALYSIS
*
82
3.5
FINITE
ELEMENT
MODEL
OF
GEOMETRIC
NONLINEARITY
OF
BEAM-SHELL
ELEMENT
BASED
ON
CR
THEORY
-----
85
3.5.1
TANGENT
STIFFNESS
MATRIX
DERIVATION
OF
TWO-DIMENSIONAL
BEAM
ELEMENT
*
85
3.5.2
DERIVATION
OF
TANGENT
STIFFNESS
MATRIX
FOR
A
THREE-DIMENSIONAL
SHELL
ELEMENT
BASED
ON
CR
METHOD
*
89
3.6
SOLUTION
OF
NONLINEAR
FINITE
ELEMENT
EQUATIONS
*
93
3.6.1
NONLINEAR
SOLUTION
TECHNIQUE
FOR
STRUCTURAL
STATIC
ANALYSIS
*
95
3.6.2
NONLINEAR
SOLUTION
TECHNOLOGY
FOR
STRUCTURAL
DYNAMIC
ANALYSIS
*
97
3.6.3
NUMERICAL
ANALYSIS
*
106
BIBLIOGRAPHY
-----
113
CHAPTER 4
INTERPOLATION
AND
MOVING-GRID
TECHNIQUE
FOR
CFD/CSD
COUPLING
PROGRAM
*
115
4.1
INTRODUCTION
*
115
4.2
INTERPOLATION
METHODS
-----
117
4.2.1
INFINITE-PLATE
SPLINES
METHOD
*
118
CONTENTS
*
IX
4.2.2
4.2.3
4.2.4
4.2.5
4.2.6
4.2.7
4.3
4.3.1
FINITE-PLATE
SPLINES
METHOD
*
119
MULTIQUADRIC-BIHARMONIC
METHOD
-----
120
THIN-PLATE
SPLINES
METHOD
*
120
INVERSE
ISOPARAMETRIC
MAPPING
METHOD
*
121
NONUNIFORM
B
SPLINES
-----
121
SPATIAL
INTERPOLATION
OF
LOAD
PARAMETERS
*
121
COUPLING
INTERFACE
DESIGN
*
121
INTERFACE
MAPPING
BASED
ON
CONSTANT
VOLUME
TRANSFORMATION
METHOD
-----
122
4.3.2
4.3.3
4.4
4.4.1
4.4.2
4.4.3
4.4.4
4.4.5
INTERFACE
MAPPING
BASED
ON
BOUNDARY
ELEMENT
METHOD
*
129
NUMERICAL
EXAMPLES
*
134
MOVING-GRID
TECHNIQUE
-----
144
GEOMETRIC
INTERPOLATION
METHOD
*
145
TRANSFINITE
INTERPOLATION
METHOD
*
147
RADIAL
BASIS
FUNCTION
METHOD
*
149
SHAPE-PRESERVING
MOVING-GRID
METHOD
*
154
NUMERICAL
EXAMPLE
OF
MOVING-GRID
TECHNIQUES
*
157
BIBLIOGRAPHY
-----
163
CHAPTER
5
CFD/CSD
COUPLING
SOLUTION
TECHNOLOGY
*
169
5.1
5.2
INTRODUCTION
-----
169
ACCURACY
ANALYSIS
OF
THE
COMMON
CFD/CSD
COUPLING
ALGORITHMS
*
170
5.2.1
5.2.2
5.3
5.3.1
5.3.2
5.4
5.4.1
5.4.2
INTRODUCTION
TO
THE
COMMON
COUPLING
ALGORITHMS
*
170
ACCURACY
ANALYSIS
BASED
ON
ENERGY
TRANSFER
*
174
THE
DESIGN
OF
THE
HIGH-ACCURACY
CFD/CSD
COUPLING
ALGORITHM
-----
180
IMPROVED
COUPLING
ALGORITHM
DESIGN
*
180
TIME-ACCURACY
ANALYSIS
OF
THE
IMPROVED
COUPLING
ALGORITHM
*
184
NUMERICAL
EXAMPLE
OF
THE
CFD/CSD
COUPLING
ALGORITHM
-----
185
ISOGAI
WING
PROFILE
AEROELASTIC
SIMULATION
*
185
AEROELASTIC
RESPONSE
ANALYSIS
OF
AGARD
445.6
WING
-----
187
BIBLIOGRAPHY
-----
192
CHAPTERS
6
REDUCED-ORDER
MODELING
TECHNIQUES
OF
NONLINEAR AEROELASTIC
SYSTEM
*
195
6.1
6.2
INTRODUCTION
-----
195
REDUCED-ORDER
MODEL
OF
UNSTEADY
AERODYNAMIC
FORCE
BASED
ON
VOLTERRA
SERIES
*
196
6.2.1
6.2.2
6.2.3
MULTIWAVELET
AND
MULTIRESOLUTION
ANALYSIS
*
196
PIECEWISE
QUADRATIC
ORTHOGONAL
MULTIWAVELET
METHOD
*
197
BOUNDARY-ADAPTIVE
SCALING
FUNCTION
AND
WAVELET
*
204
X
*
CONTENTS
6.2.4
6.2.5
6.2.6
ORTHOGONAL
MULTIWAVELET
MULTIRESOLUTION
ANALYSIS
*
205
VOLTERRA
KERNEL
APPROXIMATION
*
209
ADAPTIVE
QR
DECOMPOSITION
RECURSIVE
LEAST
SQUARES
ALGORITHM
*
214
6.2.7
6.3
6.3.1
6.3.2
6.3.3
6.4
NUMERICAL
EXAMPLES
*
216
ROMS
FOR
UNSTEADY
AERODYNAMIC
FORCES
BASED
ON
STATE
SPACE
*
221
PULSE/ERA
METHOD
-----
222
SCI/ERA
METHOD
-----
223
NUMERICAL
EXAMPLES
*
226
REDUCED-ORDER
MODEL
OF
AEROELASTIC
SYSTEM
BASED
ON
POD
METHOD
-----
228
6.4.1
6.4.2
POD-BASED
SNAPSHOT
METHOD
*
228
REDUCED-ORDER
MODELING
OF
AEROELASTIC
SYSTEM
BASED
ON
POD
METHOD
*
230
6.5
6.5.1
6.5.2
6.5.3
6.5.4
6.6
REDUCED
ORDER
OF
AEROELASTIC
SYSTEM
BASED
ON
BPOD
METHOD
*
233
BALANCE
TRUNCATED
REDUCTION
THEORY
*
233
CONSTRUCTION
OF
TRANSFORMATION
MATRIX
*
234
THE
CONNECTION
BETWEEN
POD
SNAPSHOT
AND
GRAMIAN
MATRIX
*
235
NUMERICAL
EXAMPLES
*
236
NONLINEAR
AERODYNAMIC
REDUCTION
MODEL
BASED
ON
POD-GALERKIN
PROJECTION
*
241
6.6.1
6.6.2
6.6.3
6.6.4
6.6.5
MODIFICATION
OF
FLOW
GOVERNING EQUATION
*
242
GRID
VELOCITY
DEFINITION
*
243
POD-GALERKIN
PROJECTION
*
244
CORRECTION
METHOD
*
245
NUMERICAL
EXAMPLES
*
246
BIBLIOGRAPHY
*
250
CHAPTER
7
AEROELASTIC
SOFTWARE
APPLICATION
BASED
ON
CFD/CSD
COUPLING
METHOD
*
253
7.1
7.2
7.2.1
7.2.2
7.2.3
7.2.4
7.3
7.3.1
7.3.2
7.3.3
7.4
INTRODUCTION
-----
253
INTRODUCTION
TO
COMPUTATIONAL
AEROELASTIC
SOFTWARE
*
253
SOFTWARE
FEATURES
*
253
OVERALL
DESIGN
OF
THE
SOFTWARE
*
254
SOFTWARE
SYSTEM
FRAMEWORK
*
256
DATA
USER
AND
ITS
SUBCLASSES
*
259
SOFTWARE
USAGE
*
263
PREPROCESSING
SOFTWARE
*
263
SOLVER
INTERFACE
*
270
DATA
DISPLAY
AND
PROCESSING
*
271
AEROELASTIC
SOFTWARE
APPLICATION
BASED
ON
CFD/CSD
COUPLING
METHOD
-----
272
CONTENTS
*
XI
INDEX
*
313
7.4.1
7.4.2
7.4.3
7.4.4
7.4.5
STATIC
AEROELASTIC
ANALYSIS
OF
LARGE
ASPECT
RATIO
WINGS
*
272
SUPERSONIC
FLUTTER
ANALYSIS
OF
AERODYNAMIC
CONTROL
SURFACE
*
277
DYNAMIC
LOAD
IN
AEROELASTIC
ANALYSIS
*
283
INFLUENCE
OF
DYNAMIC
PERTURBATION
ON
AEROELASTICITY
*
290
AEROELASTIC
ANALYSIS
OF
CIVIL
AIRCRAFT
*
299
BIBLIOGRAPHY
-----
311
|
| any_adam_object | 1 |
| author | Xu, Min An, Xiaomin Kang, Wei Li, Guangning |
| author_facet | Xu, Min An, Xiaomin Kang, Wei Li, Guangning |
| author_role | aut aut aut aut |
| author_sort | Xu, Min |
| author_variant | m x mx x a xa w k wk g l gl |
| building | Verbundindex |
| bvnumber | BV047282426 |
| classification_rvk | ZO 7230 |
| ctrlnum | (OCoLC)1237113833 (DE-599)DNB1140858076 |
| discipline | Verkehr / Transport |
| format | Book |
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| id | DE-604.BV047282426 |
| illustrated | Illustrated |
| indexdate | 2024-12-24T08:43:59Z |
| institution | BVB |
| institution_GND | (DE-588)10095502-2 |
| isbn | 9783110576474 3110576473 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-032685937 |
| oclc_num | 1237113833 |
| open_access_boolean | |
| owner | DE-703 |
| owner_facet | DE-703 |
| physical | XI, 315 Seiten Illustrationen, Diagramme |
| publishDate | 2021 |
| publishDateSearch | 2021 |
| publishDateSort | 2021 |
| publisher | De Gruyter |
| record_format | marc |
| spellingShingle | Xu, Min An, Xiaomin Kang, Wei Li, Guangning Modern computational aeroelasticity Aeroelastizität (DE-588)4202469-9 gnd Numerisches Verfahren (DE-588)4128130-5 gnd |
| subject_GND | (DE-588)4202469-9 (DE-588)4128130-5 |
| title | Modern computational aeroelasticity |
| title_auth | Modern computational aeroelasticity |
| title_exact_search | Modern computational aeroelasticity |
| title_full | Modern computational aeroelasticity Min Xu, Xiaomin An, Wei Kang, Guangning Li |
| title_fullStr | Modern computational aeroelasticity Min Xu, Xiaomin An, Wei Kang, Guangning Li |
| title_full_unstemmed | Modern computational aeroelasticity Min Xu, Xiaomin An, Wei Kang, Guangning Li |
| title_short | Modern computational aeroelasticity |
| title_sort | modern computational aeroelasticity |
| topic | Aeroelastizität (DE-588)4202469-9 gnd Numerisches Verfahren (DE-588)4128130-5 gnd |
| topic_facet | Aeroelastizität Numerisches Verfahren |
| url | http://www.degruyter.com/search?f_0=isbnissn&q_0=9783110576474&searchTitles=true https://d-nb.info/1140858076/04 http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=032685937&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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