Hypersonic Flows for Reentry Problems: Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Elektronisch E-Book |
Sprache: | English |
Veröffentlicht: |
Berlin, Heidelberg
Springer Berlin Heidelberg
1991
|
Schlagworte: | |
Online-Zugang: | Volltext |
Beschreibung: | This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59 |
Beschreibung: | 1 Online-Ressource (XIII, 1230p. 1054 illus) |
ISBN: | 9783642765278 9783642765292 |
DOI: | 10.1007/978-3-642-76527-8 |
Internformat
MARC
LEADER | 00000nmm a2200000zc 4500 | ||
---|---|---|---|
001 | BV042413590 | ||
003 | DE-604 | ||
005 | 00000000000000.0 | ||
007 | cr|uuu---uuuuu | ||
008 | 150316s1991 |||| o||u| ||||||eng d | ||
020 | |a 9783642765278 |c Online |9 978-3-642-76527-8 | ||
020 | |a 9783642765292 |c Print |9 978-3-642-76529-2 | ||
024 | 7 | |a 10.1007/978-3-642-76527-8 |2 doi | |
035 | |a (OCoLC)905376882 | ||
035 | |a (DE-599)BVBBV042413590 | ||
040 | |a DE-604 |b ger |e aacr | ||
041 | 0 | |a eng | |
049 | |a DE-91 |a DE-83 | ||
082 | 0 | |a 530.15 |2 23 | |
084 | |a PHY 000 |2 stub | ||
100 | 1 | |a Désidéri, Jean-Antoine |e Verfasser |4 aut | |
245 | 1 | 0 | |a Hypersonic Flows for Reentry Problems |b Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 |c edited by Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux |
246 | 1 | 3 | |a Proceedings of a Workshop Held in Antibes, France, 22-25 January 1990 |
264 | 1 | |a Berlin, Heidelberg |b Springer Berlin Heidelberg |c 1991 | |
300 | |a 1 Online-Ressource (XIII, 1230p. 1054 illus) | ||
336 | |b txt |2 rdacontent | ||
337 | |b c |2 rdamedia | ||
338 | |b cr |2 rdacarrier | ||
500 | |a This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59 | ||
650 | 4 | |a Physics | |
650 | 4 | |a Numerical analysis | |
650 | 4 | |a Mathematical physics | |
650 | 4 | |a Mathematical Methods in Physics | |
650 | 4 | |a Numerical and Computational Physics | |
650 | 4 | |a Fluid- and Aerodynamics | |
650 | 4 | |a Numerical Analysis | |
650 | 4 | |a Mathematische Physik | |
700 | 1 | |a Glowinski, Roland |e Sonstige |4 oth | |
700 | 1 | |a Périaux, Jacques |e Sonstige |4 oth | |
856 | 4 | 0 | |u https://doi.org/10.1007/978-3-642-76527-8 |x Verlag |3 Volltext |
912 | |a ZDB-2-PHA |a ZDB-2-BAE | ||
940 | 1 | |q ZDB-2-PHA_Archive | |
999 | |a oai:aleph.bib-bvb.de:BVB01-027849083 |
Datensatz im Suchindex
_version_ | 1804153078094495744 |
---|---|
any_adam_object | |
author | Désidéri, Jean-Antoine |
author_facet | Désidéri, Jean-Antoine |
author_role | aut |
author_sort | Désidéri, Jean-Antoine |
author_variant | j a d jad |
building | Verbundindex |
bvnumber | BV042413590 |
classification_tum | PHY 000 |
collection | ZDB-2-PHA ZDB-2-BAE |
ctrlnum | (OCoLC)905376882 (DE-599)BVBBV042413590 |
dewey-full | 530.15 |
dewey-hundreds | 500 - Natural sciences and mathematics |
dewey-ones | 530 - Physics |
dewey-raw | 530.15 |
dewey-search | 530.15 |
dewey-sort | 3530.15 |
dewey-tens | 530 - Physics |
discipline | Physik |
doi_str_mv | 10.1007/978-3-642-76527-8 |
format | Electronic eBook |
fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>03273nmm a2200481zc 4500</leader><controlfield tag="001">BV042413590</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">cr|uuu---uuuuu</controlfield><controlfield tag="008">150316s1991 |||| o||u| ||||||eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9783642765278</subfield><subfield code="c">Online</subfield><subfield code="9">978-3-642-76527-8</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9783642765292</subfield><subfield code="c">Print</subfield><subfield code="9">978-3-642-76529-2</subfield></datafield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/978-3-642-76527-8</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)905376882</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV042413590</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">aacr</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-91</subfield><subfield code="a">DE-83</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">530.15</subfield><subfield code="2">23</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">PHY 000</subfield><subfield code="2">stub</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Désidéri, Jean-Antoine</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Hypersonic Flows for Reentry Problems</subfield><subfield code="b">Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990</subfield><subfield code="c">edited by Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux</subfield></datafield><datafield tag="246" ind1="1" ind2="3"><subfield code="a">Proceedings of a Workshop Held in Antibes, France, 22-25 January 1990</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Berlin, Heidelberg</subfield><subfield code="b">Springer Berlin Heidelberg</subfield><subfield code="c">1991</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 Online-Ressource (XIII, 1230p. 1054 illus)</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Physics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Numerical analysis</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mathematical physics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mathematical Methods in Physics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Numerical and Computational Physics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Fluid- and Aerodynamics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Numerical Analysis</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mathematische Physik</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Glowinski, Roland</subfield><subfield code="e">Sonstige</subfield><subfield code="4">oth</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Périaux, Jacques</subfield><subfield code="e">Sonstige</subfield><subfield code="4">oth</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://doi.org/10.1007/978-3-642-76527-8</subfield><subfield code="x">Verlag</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">ZDB-2-PHA</subfield><subfield code="a">ZDB-2-BAE</subfield></datafield><datafield tag="940" ind1="1" ind2=" "><subfield code="q">ZDB-2-PHA_Archive</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-027849083</subfield></datafield></record></collection> |
id | DE-604.BV042413590 |
illustrated | Not Illustrated |
indexdate | 2024-07-10T01:20:53Z |
institution | BVB |
isbn | 9783642765278 9783642765292 |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-027849083 |
oclc_num | 905376882 |
open_access_boolean | |
owner | DE-91 DE-BY-TUM DE-83 |
owner_facet | DE-91 DE-BY-TUM DE-83 |
physical | 1 Online-Ressource (XIII, 1230p. 1054 illus) |
psigel | ZDB-2-PHA ZDB-2-BAE ZDB-2-PHA_Archive |
publishDate | 1991 |
publishDateSearch | 1991 |
publishDateSort | 1991 |
publisher | Springer Berlin Heidelberg |
record_format | marc |
spelling | Désidéri, Jean-Antoine Verfasser aut Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 edited by Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux Proceedings of a Workshop Held in Antibes, France, 22-25 January 1990 Berlin, Heidelberg Springer Berlin Heidelberg 1991 1 Online-Ressource (XIII, 1230p. 1054 illus) txt rdacontent c rdamedia cr rdacarrier This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59 Physics Numerical analysis Mathematical physics Mathematical Methods in Physics Numerical and Computational Physics Fluid- and Aerodynamics Numerical Analysis Mathematische Physik Glowinski, Roland Sonstige oth Périaux, Jacques Sonstige oth https://doi.org/10.1007/978-3-642-76527-8 Verlag Volltext |
spellingShingle | Désidéri, Jean-Antoine Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 Physics Numerical analysis Mathematical physics Mathematical Methods in Physics Numerical and Computational Physics Fluid- and Aerodynamics Numerical Analysis Mathematische Physik |
title | Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 |
title_alt | Proceedings of a Workshop Held in Antibes, France, 22-25 January 1990 |
title_auth | Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 |
title_exact_search | Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 |
title_full | Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 edited by Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux |
title_fullStr | Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 edited by Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux |
title_full_unstemmed | Hypersonic Flows for Reentry Problems Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 edited by Jean-Antoine Désidéri, Roland Glowinski, Jacques Périaux |
title_short | Hypersonic Flows for Reentry Problems |
title_sort | hypersonic flows for reentry problems volume ii test cases experiments and computations proceedings of a workshop held in antibes france 22 25 january 1990 |
title_sub | Volume II: Test Cases — Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22–25 January 1990 |
topic | Physics Numerical analysis Mathematical physics Mathematical Methods in Physics Numerical and Computational Physics Fluid- and Aerodynamics Numerical Analysis Mathematische Physik |
topic_facet | Physics Numerical analysis Mathematical physics Mathematical Methods in Physics Numerical and Computational Physics Fluid- and Aerodynamics Numerical Analysis Mathematische Physik |
url | https://doi.org/10.1007/978-3-642-76527-8 |
work_keys_str_mv | AT desiderijeanantoine hypersonicflowsforreentryproblemsvolumeiitestcasesexperimentsandcomputationsproceedingsofaworkshopheldinantibesfrance2225january1990 AT glowinskiroland hypersonicflowsforreentryproblemsvolumeiitestcasesexperimentsandcomputationsproceedingsofaworkshopheldinantibesfrance2225january1990 AT periauxjacques hypersonicflowsforreentryproblemsvolumeiitestcasesexperimentsandcomputationsproceedingsofaworkshopheldinantibesfrance2225january1990 AT desiderijeanantoine proceedingsofaworkshopheldinantibesfrance2225january1990 AT glowinskiroland proceedingsofaworkshopheldinantibesfrance2225january1990 AT periauxjacques proceedingsofaworkshopheldinantibesfrance2225january1990 |