Rotorcraft flow simulation: technology and results
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Abschlussarbeit Buch |
| Sprache: | English |
| Veröffentlicht: |
München
Verlag Dr. Hut
2019
|
| Ausgabe: | 1. Auflage |
| Schlagworte: | |
| Online-Zugang: | Inhaltstext http://www.dr.hut-verlag.de/978-3-8439-4117-4.html Inhaltsverzeichnis |
| Beschreibung: | vii, 230 Seiten Illustrationen, Diagramme 21 cm x 14.8 cm, 446 g |
| ISBN: | 9783843941174 3843941173 |
Internformat
MARC
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| 100 | 1 | |a Keßler, Manuel |e Verfasser |0 (DE-588)1196154627 |4 aut | |
| 245 | 1 | 0 | |a Rotorcraft flow simulation |b technology and results |c Manuel Keßler |
| 250 | |a 1. Auflage | ||
| 264 | 1 | |a München |b Verlag Dr. Hut |c 2019 | |
| 300 | |a vii, 230 Seiten |b Illustrationen, Diagramme |c 21 cm x 14.8 cm, 446 g | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 502 | |b Dissertation |c Universität Stuttgart |d 2018 | ||
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Datensatz im Suchindex
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|---|---|
| adam_text | CONTENTS
NOMENCLATURE
V
1
PREFACE
1
1.1
FOREWORD
...........................................
1
1.2
ABSTRACT
................................................................................................................................
2
1.3
ZUSAMMENFASSUNG
..................
3
2
INTRODUCTION
17
2.1
HISTORICAL
DEVELOPMENT
...........................................................
.
....................................
17
2.2
SIMULATION
.............................................................................................................................
18
MOMENTUM
THEORY
.................................................................................................
19
BLADE
ELEMENT
THEORY
.............................................................................................
19
VORTEX
METHODS
................................................................................................
19
COMPUTATIONAL
FLUID
DYNAMICS
...........................................
20
METHOD
SELECTION
....................................................................................................
20
...................................................................................................................................
22
23
.....................
23
3.2
CONCEPTS
........................
23
3.3
CONFIGURATIONS
....................................................................................................................
24
4
FLIGHT
PHYSICS
29
4.1
BASIC
MOMENTUM
THEORY
....................................................................................................
29
4.2 HOVER
AND
VERTICAL
FLIGHT
....................................................................................................
31
4.2.1
CLIMB
......................................................................................................
32
4.2.2
CLASSIC
CONFIGURATION
.............................................................................
33
4.2.3
MULTI-ROTOR
CONFIGURATIONS
....................................................................................
34
4.3
FORWARD
FLIGHT
......................................................................................................................
34
4.3.1
POWER
......................................................................................................................
35
4.3.2
CONTROL
AND
STEERING
...................................................................................
37
4.4
BLADE
DYNAMICS
...................................................................................................................
38
4.5
BLADE
DEFORMATIONS
..................................
40
4.6
TYIM
............................................................................................................
41
4.7
GROUND
EFFECT
........................................
41
4.8
MORE
HELICOPTER
SPECIFIC
PHENOMENA
.................................................................................
44
4.8.1
BLADE-VORTEX-INTERACTION
.......................................................................
44
4.8.2
VORTEX
RING
STATE
(VRS)
....................................................................
46
4.8.3
HIGH-G
FLIGHT
AND
MANEUVER
.
.
.....................................
48
4.8.4
DYNAMIC
STALL
.......................................................................
.
......................... ...
49
4.8.5
PITCH-UP
AND
TAIL
SHAKE
.......................................................................................
52
5
FLUID-STRUCTURE
COUPLING
55
5.1
BLADE
STRUCTURAL
MODELLING
...........................
56
5.2
STRONG
COUPLING
..................................
-
...........................
........
58
2.2.1
2.2.2
2.2.3
2.2.4
2.2.5
2.3
GOALS
3
ROTORCRAFT
3.1
5.3
WEAK
COUPLING
...................................................................................................................
59
5.4
AIRFRAME
COUPLING
................................................................................................................
60
5.4.1
STRUCTURAL
MODEL
....................................................................................................
60
5.4.2
COUPLING
FRAMEWORK
..............................................................................................
62
5.4.3
VIBRATIONS
................................................................................................................
63
5.5
ASSESSMENT
..........................................................................................................................
64
6
TRIM
65
6.1
TRIM
OBJECTIVES
AND
CONTROLS
..............................................................................................
65
6.2
UPDATE
DIRECTION
................................................................................................................
66
6.3
TYIM
CONVERGENCE
................................................................................................................
68
6.4
DEGREES
OF
FREEDOM
.............................................................................................................
72
6.5
MANEUVER
.............................................................................................................................
72
6.6
ASSESSMENT
..........................................................................................................................
73
7
BLADE
ELEMENT
THEORY
(BEM)
75
7.1
BASICS
...................................................................................................................................
75
7.2
INFLOW
...................................................................................................................................
76
7.3
EMPIRICAL
IMPROVEMENTS
....................................................................................................
79
7.4
USAGE
AND
RESULTS
................................................................................................................
80
7.5
ASSESSMENT
..........................................................................................................................
80
8
VORTEX
METHODS
83
8.1
BASICS
...................................................................................................................................
84
8.2
IMPLEMENTATION
...................................................................................................................
84
8.2.1
WAKE
......................................................................................................................
85
8.2.2
VORTEX
MODEL
..........................................................................................................
85
8.2.3
RESOLUTION
AND
CONVERGENCE
.................................................................................
86
8.2.4
SIMULATION
ACCELERATION
.......................................................................................
87
8.3
RESULTS
...................................................................................................................................
87
8.3.1
ISOLATED
ROTOR
IN
FORWARD
FLIGHT
...........................................................................
88
8.3.2
COMPOUND
(X
3
)
....................................................................................................
89
8.4
ASSESSMENT
.......................................................................
90
9
COMPUTATIONAL
FLUID
DYNAMICS
(CFD)
91
9.1
STATE
OF
THE
ART
...................................................................................................................
92
9.2
BASICS
...................................................................................................................................
93
9.2.1
GOVERNING
EQUATIONS
.............................................................................................
93
9.2.2
SCALING
ANALYSIS
.......................................................................................................
94
9.2.3
TURBULENCE
.................................................................................................................
95
9.3
DISCRETIZATION
AND
SETUPS
................................................................................................
97
9.3.1
FINITE
VOLUME
METHOD
(FVM)
..................................................................................
98
9.3.2
CHIMERA
TECHNOLOGY
AND
GRID
MOTION
.................................................................
99
9.3.3
GRID
DEFORMATION
......................................................................................................
101
9.3.4
PERIODICITY
...............................................................................................................
103
9.3.5
BOUNDARY
CONDITIONS
................................................................................................
104
9.3.6
ORDER
OF
ACCURACY
...................................................................................................
105
9.3.7
VORTEX
CONSERVATION
................................................................................................
106
9.3.8
WENO
METHOD
FOR
ORDER
IMPROVEMENT
.................................................................
109
9.3.9
BACKGROUND
GRID
......................................................................................................
112
9.3.10
AUTOMATIC
MESH
REFINEMENT
(AMR)
....................................................................
114
II
9.3.11
HYBRID
MESHES
..........................................................................................................
118
9.4
EXEMPLARY
SIMULATION
RESULTS
ON
VARIOUS
CONFIGURATIONS
.................................................
119
9.4.1
ISOLATED
ROTOR
............................................................................................................
119
9.4.2
FULL
CONFIGURATION
IN
WIND
TUNNEL
..........................................................................
119
9.4.3
OTHER
ROTOR-AIRFRAME
CONFIGURATIONS
.......................................................................
123
9.4.4
FULL
CONFIGURATION
IN
FREE
FLIGHT
.............................................................................
124
9.4.5
ENGINE
FLOW
...............................................................................................................
126
9.4.6
FLEXIBLE
AIRFRAME
......................................................................................................
127
9.4.7
COMPOUND
HELICOPTER
.............................................................................................
132
9.5
OPTIMIZATION
.........................................................................................................................
137
9.5.1
PARAMETER
DEFINITION
AND
CONSTRAINTS
....................................................................
137
9.5.2
GOALS
AND
EVALUATION
................................................................................................
137
9.5.3
SELECTION
OF
VARIANTS
AND
PARAMETER
SPACE
COVERAGE
...........................................
139
9.5.4
MANUAL
VS.
AUTOMATIC
OPTIMIZATION
.......................................................................
140
9.5.5
INTERPOLATION
AND
ACCELERATION
.......................................
141
9.5.6
BLADE
PLANFORM
OPTIMIZATION
................................................................................
142
9.6
ASSESSMENT
............................................................................................................................
143
10
DISCONTINUOUS
GALERKIN
METHOD
(DG)
145
10.1
STATE
OF
THE
ART
......................................................................................................................
145
10.2
MOTIVATION
...............................................................................................................................
146
10.3
DISCRETIZATION
.........................................................................................................................
146
10.4
METHOD
SPECIFICS
..................................................................................................................
148
10.4.1
VISCOSITY
......................................................................................................................
148
10.4.2
TURBULENCE
MODELLING
.............................................................................................
149
10.4.3
ADAPTATION
...............................................................................................................
150
10.4.4
MESH
MOTION
AND
DEFORMATION
................................................................................
150
10.4.5
CHIMERA
INTERPOLATION
.............................................................................................
151
10.4.6
SURFACE
CURVATURE
......................................................................................................
152
10.5
RESULTS
.....................................................................................................................................
154
10.5.1
AIRFOIL
SECTION
............................................................................................................
154
10.5.2
ROTOR
IN
HOVER
.........................................................................................................
154
10.5.3
RIGID
ROTOR
IN
FORWARD
FLIGHT
...................................................................................
157
10.6
ASSESSMENT
............................................................................................................................
157
11
AEROACOUSTICS
161
11.1
STATE
OF
THE
ART
.....................................................................................................................
161
11.2
ALTERNATIVE
APPROACHES
.........................................................................................................
162
11.3
ACOUSTIC
ANALOGY
..................................................................................................................
162
11.3.1
PHYSICAL
INTEGRATION
SURFACE
...................................................................................
164
11.3.2
LINE
LOADS
..................................................................................................................
164
11.3.3
CRITIQUE
.....................................................................................................................
165
11.4
TRANSPORT
...............................................................................................................................
165
11.4.1
INTEGRATION
.........................................................................................
166
11.4.2
TIME
AVERAGING
.........................................................................................................
168
11.4.3
SOURCE
TIME
APPROACH
.............................................................................................
169
11.4.4
MOVING
OBSERVER
......................................................................................................
175
11.4.5
WIND
TUNNEL
CONDITIONS
.........................................................................................
177
11.5
APPLICATION
ISSUES
..................................................................................................................
177
11.5.1
REQUIREMENTS
ON
CFD
.............................................................................................
177
11.5.2
MANEUVER
FLIGHT
.......................................................................
178
III
11.5.3
INTEGRATION
SURFACE
SELECTION
....................................................................................
180
11.5.4
SHADING
AND
REFLECTION
.............................................................................................
182
11.5.5
OTHER
NOISE
SOURCES
...........................................
184
11.6
RESULTS
.....................................................................................................................................
184
11.6.1
FREE-WAKE
-
ISOLATED
ROTOR
.......................................................................................
184
11.6.2
CFD
-
ISOLATED
ROTOR
.............................................................................................
186
11.6.3
TIP
SHAPE
OPTIMIZATION
..........................................................................................
187
11.6.4
FULL
CONFIGURATION
...................................................................................................
188
11.6.5
COMPOUND
CONFIGURATION
..........................................................................................
192
11.7
CONTRA-ROTATING
OPEN
ROTOR
(CROR)
................................................................................
193
11.8
TRAILING
EDGE
DEVICE
(MINI-TED)
.......................................................................................
196
11.9
ASSESSMENT
............................................................................................................................
198
12
CONCLUSION
199
12.1
STATUS
.....................................................................................................................................
199
12.2
SUMMARY
...............................................................................................................................
199
12.3
OUTLOOK
..................................................................................................................................
200
BIBLIOGRAPHY
201
IV
|
| any_adam_object | 1 |
| author | Keßler, Manuel |
| author_GND | (DE-588)1196154627 |
| author_facet | Keßler, Manuel |
| author_role | aut |
| author_sort | Keßler, Manuel |
| author_variant | m k mk |
| building | Verbundindex |
| bvnumber | BV046254917 |
| classification_tum | MTA 309 VER 562 |
| ctrlnum | (OCoLC)1128850615 (DE-599)DNB1192988639 |
| discipline | Maschinenbau / Maschinenwesen Physik Verkehrstechnik |
| edition | 1. Auflage |
| format | Thesis Book |
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| genre | (DE-588)4113937-9 Hochschulschrift gnd-content |
| genre_facet | Hochschulschrift |
| id | DE-604.BV046254917 |
| illustrated | Illustrated |
| indexdate | 2024-07-10T08:39:40Z |
| institution | BVB |
| institution_GND | (DE-588)10174118-2 |
| isbn | 9783843941174 3843941173 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-031633048 |
| oclc_num | 1128850615 |
| open_access_boolean | |
| owner | DE-91 DE-BY-TUM DE-12 DE-29T |
| owner_facet | DE-91 DE-BY-TUM DE-12 DE-29T |
| physical | vii, 230 Seiten Illustrationen, Diagramme 21 cm x 14.8 cm, 446 g |
| publishDate | 2019 |
| publishDateSearch | 2019 |
| publishDateSort | 2019 |
| publisher | Verlag Dr. Hut |
| record_format | marc |
| spelling | Keßler, Manuel Verfasser (DE-588)1196154627 aut Rotorcraft flow simulation technology and results Manuel Keßler 1. Auflage München Verlag Dr. Hut 2019 vii, 230 Seiten Illustrationen, Diagramme 21 cm x 14.8 cm, 446 g txt rdacontent n rdamedia nc rdacarrier Dissertation Universität Stuttgart 2018 Strömungsakustik (DE-588)4116645-0 gnd rswk-swf Diskontinuierliche Galerkin-Methode (DE-588)4588309-9 gnd rswk-swf Hubschrauber (DE-588)4025993-6 gnd rswk-swf Numerische Strömungssimulation (DE-588)4690080-9 gnd rswk-swf Wirbelströmung (DE-588)4190007-8 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Rotorblatt (DE-588)4286652-2 gnd rswk-swf Hubschrauberrotor (DE-588)4160722-3 gnd rswk-swf Hardback Helicopter Aerodynamics Simulation 1686: Hardcover, Softcover / Technik/Luftfahrttechnik, Raumfahrttechnik (DE-588)4113937-9 Hochschulschrift gnd-content Hubschrauber (DE-588)4025993-6 s Aerodynamik (DE-588)4000589-6 s Hubschrauberrotor (DE-588)4160722-3 s Rotorblatt (DE-588)4286652-2 s Wirbelströmung (DE-588)4190007-8 s Numerische Strömungssimulation (DE-588)4690080-9 s Diskontinuierliche Galerkin-Methode (DE-588)4588309-9 s Strömungsakustik (DE-588)4116645-0 s DE-604 Verlag Dr. Hut (München) (DE-588)10174118-2 pbl X:MVB text/html http://deposit.dnb.de/cgi-bin/dokserv?id=d9513ed1a83247c1a17c2e5d158025dc&prov=M&dok_var=1&dok_ext=htm Inhaltstext X:MVB http://www.dr.hut-verlag.de/978-3-8439-4117-4.html DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=031633048&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Keßler, Manuel Rotorcraft flow simulation technology and results Strömungsakustik (DE-588)4116645-0 gnd Diskontinuierliche Galerkin-Methode (DE-588)4588309-9 gnd Hubschrauber (DE-588)4025993-6 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Wirbelströmung (DE-588)4190007-8 gnd Aerodynamik (DE-588)4000589-6 gnd Rotorblatt (DE-588)4286652-2 gnd Hubschrauberrotor (DE-588)4160722-3 gnd |
| subject_GND | (DE-588)4116645-0 (DE-588)4588309-9 (DE-588)4025993-6 (DE-588)4690080-9 (DE-588)4190007-8 (DE-588)4000589-6 (DE-588)4286652-2 (DE-588)4160722-3 (DE-588)4113937-9 |
| title | Rotorcraft flow simulation technology and results |
| title_auth | Rotorcraft flow simulation technology and results |
| title_exact_search | Rotorcraft flow simulation technology and results |
| title_full | Rotorcraft flow simulation technology and results Manuel Keßler |
| title_fullStr | Rotorcraft flow simulation technology and results Manuel Keßler |
| title_full_unstemmed | Rotorcraft flow simulation technology and results Manuel Keßler |
| title_short | Rotorcraft flow simulation |
| title_sort | rotorcraft flow simulation technology and results |
| title_sub | technology and results |
| topic | Strömungsakustik (DE-588)4116645-0 gnd Diskontinuierliche Galerkin-Methode (DE-588)4588309-9 gnd Hubschrauber (DE-588)4025993-6 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Wirbelströmung (DE-588)4190007-8 gnd Aerodynamik (DE-588)4000589-6 gnd Rotorblatt (DE-588)4286652-2 gnd Hubschrauberrotor (DE-588)4160722-3 gnd |
| topic_facet | Strömungsakustik Diskontinuierliche Galerkin-Methode Hubschrauber Numerische Strömungssimulation Wirbelströmung Aerodynamik Rotorblatt Hubschrauberrotor Hochschulschrift |
| url | http://deposit.dnb.de/cgi-bin/dokserv?id=d9513ed1a83247c1a17c2e5d158025dc&prov=M&dok_var=1&dok_ext=htm http://www.dr.hut-verlag.de/978-3-8439-4117-4.html http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=031633048&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT keßlermanuel rotorcraftflowsimulationtechnologyandresults AT verlagdrhutmunchen rotorcraftflowsimulationtechnologyandresults |