Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions:
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Köln
1994
|
Ausgabe: | Als Ms. gedr. |
Schriftenreihe: | Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht
1994,36 |
Online-Zugang: | Inhaltsverzeichnis |
Beschreibung: | Zsfassung in dt. Sprache |
Beschreibung: | 108 S. graph. Darst. |
Internformat
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100 | 1 | |a Streit, Thomas |e Verfasser |4 aut | |
245 | 1 | 0 | |a Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions |c Th. Streit ; S. Martin ; Th. Eggers |
250 | |a Als Ms. gedr. | ||
264 | 1 | |a Köln |c 1994 | |
300 | |a 108 S. |b graph. Darst. | ||
336 | |b txt |2 rdacontent | ||
337 | |b n |2 rdamedia | ||
338 | |b nc |2 rdacarrier | ||
490 | 1 | |a Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |v 1994,36 | |
500 | |a Zsfassung in dt. Sprache | ||
700 | 1 | |a Martin, Sébastien |e Verfasser |4 aut | |
700 | 1 | |a Eggers, Thino |e Verfasser |4 aut | |
830 | 0 | |a Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |v 1994,36 |w (DE-604)BV002197965 |9 1994,36 | |
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=006848607&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |3 Inhaltsverzeichnis |
Datensatz im Suchindex
_version_ | 1805067306129162240 |
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adam_text |
CONTENT?
CONTENTS
.
5
LIST
OF
SYMBOLS
.
7
1.
INTRODUCTION
.
11
2.
NUMERICAL
METHOD
FOR
THE
SOLUTION
OF
THE
NAVIER-STOKES
EQUATIONS
.
13
2.1
GOVERNING
EQUATIONS
.
13
2.2
SOLUTION
METHOD
.
15
2.2.1
FIRST-ORDER
SPATIAL
DISCRETIZATION
.
15
2.2.2
SCALING
OF
THE
ADAPTIVE
DISSIPATION
FOR
VISCOUS
FLOWS
.
18
2.2.3
HIGH-ORDER
SCHEME
.
19
2.2.4
TIME
INTEGRATION
.
19
3.
SURFACE
INCLINATION
METHOD
SOSE
.
20
3.1
NEWTONIAN
THEORY
.
20
3.1.1
NEWTONIAN
THEORY
FOR
BLUNT
BODIES
.
21
3.1.2
NEWTONIAN
THEORY
FOR
A
SWEPT
CYLINDER
.
23
3.1.3
SHOCK-EXPANSION
METHOD
.
25
4.
AERODYNAMIC
HEAT
TRANSFER
.
27
4.1
HEAT
TRANSFER
COEFFICIENT
.
21
4.2
FLAT
PLATE
.
28
4.2.1
REFERENCE
TEMPERATURE
METHOD
.
29
4.2.2
VAN
DRIEST
FLAT
PLATE
THEORY
FOR
COMPRESSIBLE
TURBULENT
FLOW
.
29
4.2.3
WHITE
'
S
AND
CHRISTOPH
'
S
COMPRESSIBLE
FLAT
PLATE
RESULT:
.
30
4.3
APPROXIMATE
HEAT
TRANSFER
METHODS
FOR
AXISYMMETRIC
BODIES
.
31
4.3.1
STAGNATION
POINT
:
FAY-RIDDELL
'
S
EQUATION
.
31
4.3.2
ZOBY
'
S
EQUATION
.
32
4.3.3
LEES
EQUATION
.
34
4.4
APPROXIMATE
HEAT
TRANSFER
METHODS
FOR
BLUNT
LEADING
EDGES
.
35
4.4.1
STAGNATION
LINE
.
35
4.4.2
FIN
HEAT
TRANSFER
DISTRIBUTION
.
36
4.5
EXTENSION
OF
FLAT
PLATE
THEORY
TO
CONICAL
SURFACES
.
37
4.6
HEAT
TRANSFER
ACROSS
JUNCTIONS
.
37
4.6.1
FLAT
PLATE
-
CONE
SECTION
JUNCTION
.
38
4.6.2
JUNCTION
TO
A
BLUNT
NOSE
.
39
4.6.3
JUNCTION
TO
A
BLUNT
LEADING
EDGE
.
39
4.7
COMPUTATION
OF
RADIATION-ADIABATIC
TEMPERATURE
.
40
6
4.8
FURTHER
EXTENSIONS
TO
THE
APPROXIMATE
HEAT
TRANSFER
METHODS
.
41
5.
NUMERICAL
RESULTS
.
42
5.1
RESULTS
OBTAINED
BY
USING
FLAT
PLATE
APPROXIMATION
METHODS
.
42
5.1.1
RESULTS
FOR
THE
HYPERSONIC
MISSILE
CONFIGURATION
.
43
5.1.2
RESULTS
FOR
THE
WAVERIDER
CONFIGURATION
.
41
5.2
RESULT
FOR
BLUNT-NOSE
CONFIGURATIONS
AND
A
BLUNT
FIN
.
46
5.2.1
FLOW
CONDITIONS,
GEOMETRY
DEFINITION
AND
MESH
GENERATION:
.
46
5.2.2
RESULTS
FOR
THE
BLUNT
BODIES
.
47
5.2.2.1
CASES
WITH
LAMINAR
BOUNDARY
LAYER
:
.
48
5.2.2.2
CASE
WITH
TRANSITION
TO
TURBULENT
BOUNDARY
LAYER
.
49
5.2.3
RESULTS
FOR
THE
FIN
.
3)
5.2.4
RESULTS
FOR
A
COMPLETE
MISSILE
CONFIGURATION
.
50
6.
CONCLUSIONS
.
52
7.
REFERENCES
.
55
8.
FIGURES
.
59
APPENDIX:
USER
NOTES
FOR
PROGRAM
HOTSOSE
.
99 |
any_adam_object | 1 |
author | Streit, Thomas Martin, Sébastien Eggers, Thino |
author_facet | Streit, Thomas Martin, Sébastien Eggers, Thino |
author_role | aut aut aut |
author_sort | Streit, Thomas |
author_variant | t s ts s m sm t e te |
building | Verbundindex |
bvnumber | BV010294349 |
ctrlnum | (OCoLC)75586263 (DE-599)BVBBV010294349 |
edition | Als Ms. gedr. |
format | Book |
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id | DE-604.BV010294349 |
illustrated | Illustrated |
indexdate | 2024-07-20T03:32:07Z |
institution | BVB |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-006848607 |
oclc_num | 75586263 |
open_access_boolean | |
owner | DE-12 DE-91G DE-BY-TUM DE-210 DE-M122 DE-83 |
owner_facet | DE-12 DE-91G DE-BY-TUM DE-210 DE-M122 DE-83 |
physical | 108 S. graph. Darst. |
publishDate | 1994 |
publishDateSearch | 1994 |
publishDateSort | 1994 |
record_format | marc |
series | Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |
series2 | Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |
spelling | Streit, Thomas Verfasser aut Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions Th. Streit ; S. Martin ; Th. Eggers Als Ms. gedr. Köln 1994 108 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht 1994,36 Zsfassung in dt. Sprache Martin, Sébastien Verfasser aut Eggers, Thino Verfasser aut Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht 1994,36 (DE-604)BV002197965 1994,36 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=006848607&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
spellingShingle | Streit, Thomas Martin, Sébastien Eggers, Thino Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions Deutsche Forschungsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |
title | Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions |
title_auth | Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions |
title_exact_search | Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions |
title_full | Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions Th. Streit ; S. Martin ; Th. Eggers |
title_fullStr | Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions Th. Streit ; S. Martin ; Th. Eggers |
title_full_unstemmed | Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions Th. Streit ; S. Martin ; Th. Eggers |
title_short | Approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical Navier-Stokes solutions |
title_sort | approximate heat transfer methods for hypersonic flow in comparison with results provided by numerical navier stokes solutions |
url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=006848607&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
volume_link | (DE-604)BV002197965 |
work_keys_str_mv | AT streitthomas approximateheattransfermethodsforhypersonicflowincomparisonwithresultsprovidedbynumericalnavierstokessolutions AT martinsebastien approximateheattransfermethodsforhypersonicflowincomparisonwithresultsprovidedbynumericalnavierstokessolutions AT eggersthino approximateheattransfermethodsforhypersonicflowincomparisonwithresultsprovidedbynumericalnavierstokessolutions |