Experimental analysis of shock-acoustic-wave interaction in transonic flow:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Abschlussarbeit Buch |
| Sprache: | English |
| Veröffentlicht: |
Aachen
Verlagshaus Mainz GmbH
2020
|
| Ausgabe: | 1. Auflage |
| Schriftenreihe: | Aachener Beiträge zur Strömungsmechanik
16 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | xv, 106 Seiten 58 Illustrationen 21 cm x 14.8 cm, 178 g |
| ISBN: | 9783958863668 3958863663 |
Internformat
MARC
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| 100 | 1 | |a Feldhusen-Hoffmann, Antje |e Verfasser |0 (DE-588)1216200378 |4 aut | |
| 245 | 1 | 0 | |a Experimental analysis of shock-acoustic-wave interaction in transonic flow |c Antje Feldhusen-Hoffmann |
| 250 | |a 1. Auflage | ||
| 263 | |a 202008 | ||
| 264 | 1 | |a Aachen |b Verlagshaus Mainz GmbH |c 2020 | |
| 300 | |a xv, 106 Seiten |b 58 Illustrationen |c 21 cm x 14.8 cm, 178 g | ||
| 336 | |b txt |2 rdacontent | ||
| 336 | |b sti |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 1 | |a Aachener Beiträge zur Strömungsmechanik |v 16 | |
| 502 | |b Dissertation |c Rheinisch-Westfälische Technische Hochschule Aachen |d 2019 | ||
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| 650 | 0 | 7 | |a Oszillierende Strömung |0 (DE-588)4279456-0 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Particle-Image-Velocimetry |0 (DE-588)4333165-8 |2 gnd |9 rswk-swf |
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| 653 | |a Schwingungen | ||
| 653 | |a Tragflügel | ||
| 653 | |a Akustik | ||
| 653 | |a Mechanik | ||
| 653 | |a Schallwellen | ||
| 653 | |a Flügel | ||
| 653 | |a Technik | ||
| 653 | |a Stoßwellen | ||
| 653 | |a Wellen | ||
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Datensatz im Suchindex
| _version_ | 1804181777746493441 |
|---|---|
| adam_text | CONTENTS
DANKSAGUNG
III
ABSTRACT
V
ZUSAMMENFASSUNG
VII
NOMENCLATURE
XI
1
INTRODUCTION
1
2
TRANSONIC
AIRFOIL
BUFFET
5
2.1
THEORIES
ABOUT
THE
MECHANISMS
OF
SELF-SUSTAINED
SHOCK
WAVE
OSCILLATIONS
...
7
2.2
OBJECTIVES
OF
THE
CURRENT
WORK
............................................................................
15
2.3
OUTLINE
....................................................................................................................
16
3
EXPERIMENTAL
FACILITIES
19
3.1
WIND
TUNNEL
...........................................................................................................
19
3.2
ADAPTIVE
TEST
SECTION
............................................................................................
20
3.3
ARTIFICIAL
SOUND
SOURCE
.........................................................................................
22
3.4
AIRFOIL
MODEL
........................................................................................................
22
4
MEASUREMENT
TECHNIQUES
25
4.1
PRESSURE
MEASUREMENT
TECHNIQUES
......................................................................
25
4.1.1
TIME-AVERAGED
PRESSURES
.........................................................................
25
4.1.2
TIME-DEPENDENT
PRESSURES
......................................................................
26
4.2
PARTICLE-IMAGE
VELOCIMETRY
..................................................................................
26
4.2.1
GENERAL
PRINCIPLE
OF
PIV
.........................................................................
27
4.2.2
PARTICLE
LIGHT
SCATTERING
CHARACTERISTICS
.................................................
30
4.2.3
PARTICLE
TRACKING
CHARACTERISTICS
.............................................................
31
4.2.4
STEREOSCOPIC
PIV
.....................................................................................
33
4.2.5
TOMOGRAPHIC
PIV
.....................................................................................
34
4.3
EXPERIMENTAL
SETUPS
AND
DATA
PROCESSING
...........................................................
38
IX
CONTENTS
5
GENERAL
DESCRIPTION
OF
THE
DRA
2303
BUFFET
FLOW
FIELD
45
5.1
RESULTS
.....................................................................................................................
45
5.2
CONCLUDING
REMARKS
...............................................................................................
52
6
ANALYSIS
OF
VORTEX-SOUND
SOURCE
DISTRIBUTIONS
55
6.1
DESCRIPTION
OF
VORTEX-BASED
SOUND
SOURCES
WITH
THE
LAMB
VECTOR
....................
55
6.2
RESULTS
.....................................................................................................................
57
6.3
CONCLUDING
REMARKS
...............................................................................................
63
7
IMPACT
OF
ARTIFICIAL
SOUND
WAVES
65
7.1
ACOUSTIC
ENVIRONMENT
OF
THE
WIND
TUNNEL
............................................................
67
7.2
RESULTS
FOR
THE
REFERENCE
SOUND
.............................................................................
67
7.3
RESULTS
FOR
THE
VARIATION
OF
SOUND
.......................................................................
70
7.4
CONCLUDING
REMARKS
...............................................................................................
72
8
DYNAMIC
MODE
DECOMPOSITION
OF
THE
DRA
2303
BUFFET
FLOW
FIELD
75
8.1
DYNAMIC
MODE
DECOMPOSITION
.............................................................................
77
8.2
RESULTS
.....................................................................................................................
82
8.2.1
REDUCING
THE
NUMBER
OF
MODES
BY
SP-DMD
........................................
82
8.2.2
THE
BUFFET
MODE
......................................................................................
86
8.2.3
THE
VORTEX
MODE
......................................................................................
90
8.2.4
FURTHER
STABLE
MODES
................................................................................
90
8.2.5
CONCLUDING
REMARKS
...................................................................................
93
9
SUMMARY
AND
CONCLUSION
95
REFERENCES
99
|
| adam_txt |
CONTENTS
DANKSAGUNG
III
ABSTRACT
V
ZUSAMMENFASSUNG
VII
NOMENCLATURE
XI
1
INTRODUCTION
1
2
TRANSONIC
AIRFOIL
BUFFET
5
2.1
THEORIES
ABOUT
THE
MECHANISMS
OF
SELF-SUSTAINED
SHOCK
WAVE
OSCILLATIONS
.
7
2.2
OBJECTIVES
OF
THE
CURRENT
WORK
.
15
2.3
OUTLINE
.
16
3
EXPERIMENTAL
FACILITIES
19
3.1
WIND
TUNNEL
.
19
3.2
ADAPTIVE
TEST
SECTION
.
20
3.3
ARTIFICIAL
SOUND
SOURCE
.
22
3.4
AIRFOIL
MODEL
.
22
4
MEASUREMENT
TECHNIQUES
25
4.1
PRESSURE
MEASUREMENT
TECHNIQUES
.
25
4.1.1
TIME-AVERAGED
PRESSURES
.
25
4.1.2
TIME-DEPENDENT
PRESSURES
.
26
4.2
PARTICLE-IMAGE
VELOCIMETRY
.
26
4.2.1
GENERAL
PRINCIPLE
OF
PIV
.
27
4.2.2
PARTICLE
LIGHT
SCATTERING
CHARACTERISTICS
.
30
4.2.3
PARTICLE
TRACKING
CHARACTERISTICS
.
31
4.2.4
STEREOSCOPIC
PIV
.
33
4.2.5
TOMOGRAPHIC
PIV
.
34
4.3
EXPERIMENTAL
SETUPS
AND
DATA
PROCESSING
.
38
IX
CONTENTS
5
GENERAL
DESCRIPTION
OF
THE
DRA
2303
BUFFET
FLOW
FIELD
45
5.1
RESULTS
.
45
5.2
CONCLUDING
REMARKS
.
52
6
ANALYSIS
OF
VORTEX-SOUND
SOURCE
DISTRIBUTIONS
55
6.1
DESCRIPTION
OF
VORTEX-BASED
SOUND
SOURCES
WITH
THE
LAMB
VECTOR
.
55
6.2
RESULTS
.
57
6.3
CONCLUDING
REMARKS
.
63
7
IMPACT
OF
ARTIFICIAL
SOUND
WAVES
65
7.1
ACOUSTIC
ENVIRONMENT
OF
THE
WIND
TUNNEL
.
67
7.2
RESULTS
FOR
THE
REFERENCE
SOUND
.
67
7.3
RESULTS
FOR
THE
VARIATION
OF
SOUND
.
70
7.4
CONCLUDING
REMARKS
.
72
8
DYNAMIC
MODE
DECOMPOSITION
OF
THE
DRA
2303
BUFFET
FLOW
FIELD
75
8.1
DYNAMIC
MODE
DECOMPOSITION
.
77
8.2
RESULTS
.
82
8.2.1
REDUCING
THE
NUMBER
OF
MODES
BY
SP-DMD
.
82
8.2.2
THE
BUFFET
MODE
.
86
8.2.3
THE
VORTEX
MODE
.
90
8.2.4
FURTHER
STABLE
MODES
.
90
8.2.5
CONCLUDING
REMARKS
.
93
9
SUMMARY
AND
CONCLUSION
95
REFERENCES
99 |
| any_adam_object | 1 |
| any_adam_object_boolean | 1 |
| author | Feldhusen-Hoffmann, Antje |
| author_GND | (DE-588)1216200378 |
| author_facet | Feldhusen-Hoffmann, Antje |
| author_role | aut |
| author_sort | Feldhusen-Hoffmann, Antje |
| author_variant | a f h afh |
| building | Verbundindex |
| bvnumber | BV046903577 |
| classification_rvk | ZO 7230 |
| ctrlnum | (OCoLC)1225084254 (DE-599)DNB1216649642 |
| discipline | Maschinenbau / Maschinenwesen Verkehr / Transport |
| discipline_str_mv | Maschinenbau / Maschinenwesen Verkehr / Transport |
| edition | 1. Auflage |
| format | Thesis Book |
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| genre | (DE-588)4113937-9 Hochschulschrift gnd-content |
| genre_facet | Hochschulschrift |
| id | DE-604.BV046903577 |
| illustrated | Illustrated |
| index_date | 2024-07-03T15:25:17Z |
| indexdate | 2024-07-10T08:57:03Z |
| institution | BVB |
| institution_GND | (DE-588)1065499698 |
| isbn | 9783958863668 3958863663 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-032313183 |
| oclc_num | 1225084254 |
| open_access_boolean | |
| owner | DE-83 |
| owner_facet | DE-83 |
| physical | xv, 106 Seiten 58 Illustrationen 21 cm x 14.8 cm, 178 g |
| publishDate | 2020 |
| publishDateSearch | 2020 |
| publishDateSort | 2020 |
| publisher | Verlagshaus Mainz GmbH |
| record_format | marc |
| series | Aachener Beiträge zur Strömungsmechanik |
| series2 | Aachener Beiträge zur Strömungsmechanik |
| spelling | Feldhusen-Hoffmann, Antje Verfasser (DE-588)1216200378 aut Experimental analysis of shock-acoustic-wave interaction in transonic flow Antje Feldhusen-Hoffmann 1. Auflage 202008 Aachen Verlagshaus Mainz GmbH 2020 xv, 106 Seiten 58 Illustrationen 21 cm x 14.8 cm, 178 g txt rdacontent sti rdacontent n rdamedia nc rdacarrier Aachener Beiträge zur Strömungsmechanik 16 Dissertation Rheinisch-Westfälische Technische Hochschule Aachen 2019 Selbsterregte Schwingung (DE-588)4275825-7 gnd rswk-swf Transsonische Strömung (DE-588)4135633-0 gnd rswk-swf Oszillierende Strömung (DE-588)4279456-0 gnd rswk-swf Particle-Image-Velocimetry (DE-588)4333165-8 gnd rswk-swf Strömungsakustik (DE-588)4116645-0 gnd rswk-swf Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 gnd rswk-swf Tragflügelumströmung (DE-588)4185837-2 gnd rswk-swf Windkanal (DE-588)4189940-4 gnd rswk-swf Schwingungen Tragflügel Akustik Mechanik Schallwellen Flügel Technik Stoßwellen Wellen (DE-588)4113937-9 Hochschulschrift gnd-content Tragflügelumströmung (DE-588)4185837-2 s Transsonische Strömung (DE-588)4135633-0 s Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 s Selbsterregte Schwingung (DE-588)4275825-7 s Oszillierende Strömung (DE-588)4279456-0 s Strömungsakustik (DE-588)4116645-0 s Windkanal (DE-588)4189940-4 s Particle-Image-Velocimetry (DE-588)4333165-8 s DE-604 Verlag Mainz (DE-588)1065499698 pbl Aachener Beiträge zur Strömungsmechanik 16 (DE-604)BV012780166 16 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=032313183&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Feldhusen-Hoffmann, Antje Experimental analysis of shock-acoustic-wave interaction in transonic flow Aachener Beiträge zur Strömungsmechanik Selbsterregte Schwingung (DE-588)4275825-7 gnd Transsonische Strömung (DE-588)4135633-0 gnd Oszillierende Strömung (DE-588)4279456-0 gnd Particle-Image-Velocimetry (DE-588)4333165-8 gnd Strömungsakustik (DE-588)4116645-0 gnd Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 gnd Tragflügelumströmung (DE-588)4185837-2 gnd Windkanal (DE-588)4189940-4 gnd |
| subject_GND | (DE-588)4275825-7 (DE-588)4135633-0 (DE-588)4279456-0 (DE-588)4333165-8 (DE-588)4116645-0 (DE-588)4282522-2 (DE-588)4185837-2 (DE-588)4189940-4 (DE-588)4113937-9 |
| title | Experimental analysis of shock-acoustic-wave interaction in transonic flow |
| title_auth | Experimental analysis of shock-acoustic-wave interaction in transonic flow |
| title_exact_search | Experimental analysis of shock-acoustic-wave interaction in transonic flow |
| title_exact_search_txtP | Experimental analysis of shock-acoustic-wave interaction in transonic flow |
| title_full | Experimental analysis of shock-acoustic-wave interaction in transonic flow Antje Feldhusen-Hoffmann |
| title_fullStr | Experimental analysis of shock-acoustic-wave interaction in transonic flow Antje Feldhusen-Hoffmann |
| title_full_unstemmed | Experimental analysis of shock-acoustic-wave interaction in transonic flow Antje Feldhusen-Hoffmann |
| title_short | Experimental analysis of shock-acoustic-wave interaction in transonic flow |
| title_sort | experimental analysis of shock acoustic wave interaction in transonic flow |
| topic | Selbsterregte Schwingung (DE-588)4275825-7 gnd Transsonische Strömung (DE-588)4135633-0 gnd Oszillierende Strömung (DE-588)4279456-0 gnd Particle-Image-Velocimetry (DE-588)4333165-8 gnd Strömungsakustik (DE-588)4116645-0 gnd Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 gnd Tragflügelumströmung (DE-588)4185837-2 gnd Windkanal (DE-588)4189940-4 gnd |
| topic_facet | Selbsterregte Schwingung Transsonische Strömung Oszillierende Strömung Particle-Image-Velocimetry Strömungsakustik Stoß-Grenzschicht-Wechselwirkung Tragflügelumströmung Windkanal Hochschulschrift |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=032313183&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV012780166 |
| work_keys_str_mv | AT feldhusenhoffmannantje experimentalanalysisofshockacousticwaveinteractionintransonicflow AT verlagmainz experimentalanalysisofshockacousticwaveinteractionintransonicflow |