A Theory of Supercritical Wing Sections, with Computer Programs and Examples: With Computer Programs and Examples
At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and mak...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Berlin, Heidelberg
Springer Berlin Heidelberg
1972
|
| Ausgabe: | 1st ed. 1972 |
| Schriftenreihe: | Lecture Notes in Economics and Mathematical Systems
66 |
| Schlagworte: | |
| Online-Zugang: | BTU01 Volltext |
| Zusammenfassung: | At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. Another contribution is a program for the analysis of transonic flow with shocks past an airfoil at off-design conditions. In our design work we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part. In Part III and in Appendices II and III we give numerical examples and discuss computa tional results. The main substance of the report, however, is contained in the listing of the computer programs themselves in Appendix IV. We have used the Fortran language throughout and we have included numerous comment cards in the listing |
| Beschreibung: | 1 Online-Ressource (VI, 214 p) |
| ISBN: | 9783642806780 |
| DOI: | 10.1007/978-3-642-80678-0 |
Internformat
MARC
| LEADER | 00000nmm a2200000zcb4500 | ||
|---|---|---|---|
| 001 | BV046871833 | ||
| 003 | DE-604 | ||
| 005 | 00000000000000.0 | ||
| 007 | cr|uuu---uuuuu | ||
| 008 | 200828s1972 |||| o||u| ||||||eng d | ||
| 020 | |a 9783642806780 |9 978-3-642-80678-0 | ||
| 024 | 7 | |a 10.1007/978-3-642-80678-0 |2 doi | |
| 035 | |a (ZDB-2-SBE)978-3-642-80678-0 | ||
| 035 | |a (OCoLC)1193304505 | ||
| 035 | |a (DE-599)BVBBV046871833 | ||
| 040 | |a DE-604 |b ger |e aacr | ||
| 041 | 0 | |a eng | |
| 049 | |a DE-634 | ||
| 082 | 0 | |a 650 |2 23 | |
| 082 | 0 | |a 658.05 |2 23 | |
| 084 | |a SI 853 |0 (DE-625)143200: |2 rvk | ||
| 084 | |a UF 4500 |0 (DE-625)145585: |2 rvk | ||
| 100 | 1 | |a Bauer, F. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a A Theory of Supercritical Wing Sections, with Computer Programs and Examples |b With Computer Programs and Examples |c by F. Bauer, P. Garabedian, D. Korn |
| 250 | |a 1st ed. 1972 | ||
| 264 | 1 | |a Berlin, Heidelberg |b Springer Berlin Heidelberg |c 1972 | |
| 300 | |a 1 Online-Ressource (VI, 214 p) | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b c |2 rdamedia | ||
| 338 | |b cr |2 rdacarrier | ||
| 490 | 0 | |a Lecture Notes in Economics and Mathematical Systems |v 66 | |
| 520 | |a At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. Another contribution is a program for the analysis of transonic flow with shocks past an airfoil at off-design conditions. In our design work we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part. In Part III and in Appendices II and III we give numerical examples and discuss computa tional results. The main substance of the report, however, is contained in the listing of the computer programs themselves in Appendix IV. We have used the Fortran language throughout and we have included numerous comment cards in the listing | ||
| 650 | 4 | |a IT in Business | |
| 650 | 4 | |a Information technology | |
| 650 | 4 | |a Business—Data processing | |
| 650 | 0 | 7 | |a Theorie |0 (DE-588)4059787-8 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Superkritischer Flügel |0 (DE-588)4184115-3 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Flugzeug |0 (DE-588)4017672-1 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Tragflügel |0 (DE-588)4060582-6 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Superkritischer Flügel |0 (DE-588)4184115-3 |D s |
| 689 | 0 | 1 | |a Theorie |0 (DE-588)4059787-8 |D s |
| 689 | 0 | |5 DE-604 | |
| 689 | 1 | 0 | |a Tragflügel |0 (DE-588)4060582-6 |D s |
| 689 | 1 | 1 | |a Flugzeug |0 (DE-588)4017672-1 |D s |
| 689 | 1 | |5 DE-604 | |
| 700 | 1 | |a Garabedian, P. |4 aut | |
| 700 | 1 | |a Korn, D. |4 aut | |
| 776 | 0 | 8 | |i Erscheint auch als |n Druck-Ausgabe |z 9783540058076 |
| 776 | 0 | 8 | |i Erscheint auch als |n Druck-Ausgabe |z 9783642806797 |
| 856 | 4 | 0 | |u https://doi.org/10.1007/978-3-642-80678-0 |x Verlag |z URL des Erstveröffentlichers |3 Volltext |
| 912 | |a ZDB-2-SBE |a ZDB-2-BAE | ||
| 940 | 1 | |q ZDB-2-SBE_Archiv | |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-032281965 | ||
| 966 | e | |u https://doi.org/10.1007/978-3-642-80678-0 |l BTU01 |p ZDB-2-SBE |q ZDB-2-SBE_Archiv |x Verlag |3 Volltext | |
Datensatz im Suchindex
| _version_ | 1804181720103124992 |
|---|---|
| adam_txt | |
| any_adam_object | |
| any_adam_object_boolean | |
| author | Bauer, F. Garabedian, P. Korn, D. |
| author_facet | Bauer, F. Garabedian, P. Korn, D. |
| author_role | aut aut aut |
| author_sort | Bauer, F. |
| author_variant | f b fb p g pg d k dk |
| building | Verbundindex |
| bvnumber | BV046871833 |
| classification_rvk | SI 853 UF 4500 |
| collection | ZDB-2-SBE ZDB-2-BAE |
| ctrlnum | (ZDB-2-SBE)978-3-642-80678-0 (OCoLC)1193304505 (DE-599)BVBBV046871833 |
| dewey-full | 650 658.05 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 650 - Management and auxiliary services 658 - General management |
| dewey-raw | 650 658.05 |
| dewey-search | 650 658.05 |
| dewey-sort | 3650 |
| dewey-tens | 650 - Management and auxiliary services |
| discipline | Physik Mathematik Wirtschaftswissenschaften |
| discipline_str_mv | Physik Mathematik Wirtschaftswissenschaften |
| doi_str_mv | 10.1007/978-3-642-80678-0 |
| edition | 1st ed. 1972 |
| format | Electronic eBook |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>03837nmm a2200613zcb4500</leader><controlfield tag="001">BV046871833</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">cr|uuu---uuuuu</controlfield><controlfield tag="008">200828s1972 |||| o||u| ||||||eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9783642806780</subfield><subfield code="9">978-3-642-80678-0</subfield></datafield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/978-3-642-80678-0</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(ZDB-2-SBE)978-3-642-80678-0</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)1193304505</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV046871833</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-634</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">650</subfield><subfield code="2">23</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">658.05</subfield><subfield code="2">23</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">SI 853</subfield><subfield code="0">(DE-625)143200:</subfield><subfield code="2">rvk</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">UF 4500</subfield><subfield code="0">(DE-625)145585:</subfield><subfield code="2">rvk</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Bauer, F.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">A Theory of Supercritical Wing Sections, with Computer Programs and Examples</subfield><subfield code="b">With Computer Programs and Examples</subfield><subfield code="c">by F. Bauer, P. Garabedian, D. Korn</subfield></datafield><datafield tag="250" ind1=" " ind2=" "><subfield code="a">1st ed. 1972</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Berlin, Heidelberg</subfield><subfield code="b">Springer Berlin Heidelberg</subfield><subfield code="c">1972</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 Online-Ressource (VI, 214 p)</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="490" ind1="0" ind2=" "><subfield code="a">Lecture Notes in Economics and Mathematical Systems</subfield><subfield code="v">66</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. Another contribution is a program for the analysis of transonic flow with shocks past an airfoil at off-design conditions. In our design work we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part. In Part III and in Appendices II and III we give numerical examples and discuss computa tional results. The main substance of the report, however, is contained in the listing of the computer programs themselves in Appendix IV. We have used the Fortran language throughout and we have included numerous comment cards in the listing</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">IT in Business</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Information technology</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Business—Data processing</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Theorie</subfield><subfield code="0">(DE-588)4059787-8</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Superkritischer Flügel</subfield><subfield code="0">(DE-588)4184115-3</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Flugzeug</subfield><subfield code="0">(DE-588)4017672-1</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Tragflügel</subfield><subfield code="0">(DE-588)4060582-6</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Superkritischer Flügel</subfield><subfield code="0">(DE-588)4184115-3</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="1"><subfield code="a">Theorie</subfield><subfield code="0">(DE-588)4059787-8</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="1" ind2="0"><subfield code="a">Tragflügel</subfield><subfield code="0">(DE-588)4060582-6</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2="1"><subfield code="a">Flugzeug</subfield><subfield code="0">(DE-588)4017672-1</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Garabedian, P.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Korn, D.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="776" ind1="0" ind2="8"><subfield code="i">Erscheint auch als</subfield><subfield code="n">Druck-Ausgabe</subfield><subfield code="z">9783540058076</subfield></datafield><datafield tag="776" ind1="0" ind2="8"><subfield code="i">Erscheint auch als</subfield><subfield code="n">Druck-Ausgabe</subfield><subfield code="z">9783642806797</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://doi.org/10.1007/978-3-642-80678-0</subfield><subfield code="x">Verlag</subfield><subfield code="z">URL des Erstveröffentlichers</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">ZDB-2-SBE</subfield><subfield code="a">ZDB-2-BAE</subfield></datafield><datafield tag="940" ind1="1" ind2=" "><subfield code="q">ZDB-2-SBE_Archiv</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-032281965</subfield></datafield><datafield tag="966" ind1="e" ind2=" "><subfield code="u">https://doi.org/10.1007/978-3-642-80678-0</subfield><subfield code="l">BTU01</subfield><subfield code="p">ZDB-2-SBE</subfield><subfield code="q">ZDB-2-SBE_Archiv</subfield><subfield code="x">Verlag</subfield><subfield code="3">Volltext</subfield></datafield></record></collection> |
| id | DE-604.BV046871833 |
| illustrated | Not Illustrated |
| index_date | 2024-07-03T15:15:36Z |
| indexdate | 2024-07-10T08:56:08Z |
| institution | BVB |
| isbn | 9783642806780 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-032281965 |
| oclc_num | 1193304505 |
| open_access_boolean | |
| owner | DE-634 |
| owner_facet | DE-634 |
| physical | 1 Online-Ressource (VI, 214 p) |
| psigel | ZDB-2-SBE ZDB-2-BAE ZDB-2-SBE_Archiv ZDB-2-SBE ZDB-2-SBE_Archiv |
| publishDate | 1972 |
| publishDateSearch | 1972 |
| publishDateSort | 1972 |
| publisher | Springer Berlin Heidelberg |
| record_format | marc |
| series2 | Lecture Notes in Economics and Mathematical Systems |
| spelling | Bauer, F. Verfasser aut A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples by F. Bauer, P. Garabedian, D. Korn 1st ed. 1972 Berlin, Heidelberg Springer Berlin Heidelberg 1972 1 Online-Ressource (VI, 214 p) txt rdacontent c rdamedia cr rdacarrier Lecture Notes in Economics and Mathematical Systems 66 At present, there is considerable interest in supercritical wing technology for the development of aircraft designed to fly near the speed of sound. The basic principle is the suppression of boundary layer separation by shifting the shock waves that occur on the wing toward the trailing edge and making them as weak as possible. The purpose of this report is to make available to the engineering public mathematical methods for the design of supercritical wings. These methods depend on the numerical solution of the partial differential equations of two-dimensional gas dynamics. The main contribution is a computer program for the design of shockless transonic airfoils using the hodograph transformation and analytic continuation into the complex domain. Another contribution is a program for the analysis of transonic flow with shocks past an airfoil at off-design conditions. In our design work we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part. In Part III and in Appendices II and III we give numerical examples and discuss computa tional results. The main substance of the report, however, is contained in the listing of the computer programs themselves in Appendix IV. We have used the Fortran language throughout and we have included numerous comment cards in the listing IT in Business Information technology Business—Data processing Theorie (DE-588)4059787-8 gnd rswk-swf Superkritischer Flügel (DE-588)4184115-3 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Tragflügel (DE-588)4060582-6 gnd rswk-swf Superkritischer Flügel (DE-588)4184115-3 s Theorie (DE-588)4059787-8 s DE-604 Tragflügel (DE-588)4060582-6 s Flugzeug (DE-588)4017672-1 s Garabedian, P. aut Korn, D. aut Erscheint auch als Druck-Ausgabe 9783540058076 Erscheint auch als Druck-Ausgabe 9783642806797 https://doi.org/10.1007/978-3-642-80678-0 Verlag URL des Erstveröffentlichers Volltext |
| spellingShingle | Bauer, F. Garabedian, P. Korn, D. A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples IT in Business Information technology Business—Data processing Theorie (DE-588)4059787-8 gnd Superkritischer Flügel (DE-588)4184115-3 gnd Flugzeug (DE-588)4017672-1 gnd Tragflügel (DE-588)4060582-6 gnd |
| subject_GND | (DE-588)4059787-8 (DE-588)4184115-3 (DE-588)4017672-1 (DE-588)4060582-6 |
| title | A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples |
| title_auth | A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples |
| title_exact_search | A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples |
| title_exact_search_txtP | A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples |
| title_full | A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples by F. Bauer, P. Garabedian, D. Korn |
| title_fullStr | A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples by F. Bauer, P. Garabedian, D. Korn |
| title_full_unstemmed | A Theory of Supercritical Wing Sections, with Computer Programs and Examples With Computer Programs and Examples by F. Bauer, P. Garabedian, D. Korn |
| title_short | A Theory of Supercritical Wing Sections, with Computer Programs and Examples |
| title_sort | a theory of supercritical wing sections with computer programs and examples with computer programs and examples |
| title_sub | With Computer Programs and Examples |
| topic | IT in Business Information technology Business—Data processing Theorie (DE-588)4059787-8 gnd Superkritischer Flügel (DE-588)4184115-3 gnd Flugzeug (DE-588)4017672-1 gnd Tragflügel (DE-588)4060582-6 gnd |
| topic_facet | IT in Business Information technology Business—Data processing Theorie Superkritischer Flügel Flugzeug Tragflügel |
| url | https://doi.org/10.1007/978-3-642-80678-0 |
| work_keys_str_mv | AT bauerf atheoryofsupercriticalwingsectionswithcomputerprogramsandexampleswithcomputerprogramsandexamples AT garabedianp atheoryofsupercriticalwingsectionswithcomputerprogramsandexampleswithcomputerprogramsandexamples AT kornd atheoryofsupercriticalwingsectionswithcomputerprogramsandexampleswithcomputerprogramsandexamples |