Computerized buckling analysis of shells:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Dordrecht
Springer Netherlands
1989
|
| Schriftenreihe: | Mechanics of Elastic Stability
9 |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Beschreibung: | This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways |
| Beschreibung: | 1 Online-Ressource (XVII, 423 p) |
| ISBN: | 9789400950634 9789401087414 |
| ISSN: | 0924-2112 |
| DOI: | 10.1007/978-94-009-5063-4 |
Internformat
MARC
| LEADER | 00000nmm a2200000zcb4500 | ||
|---|---|---|---|
| 001 | BV042415206 | ||
| 003 | DE-604 | ||
| 005 | 00000000000000.0 | ||
| 007 | cr|uuu---uuuuu | ||
| 008 | 150316s1989 |||| o||u| ||||||eng d | ||
| 020 | |a 9789400950634 |c Online |9 978-94-009-5063-4 | ||
| 020 | |a 9789401087414 |c Print |9 978-94-010-8741-4 | ||
| 024 | 7 | |a 10.1007/978-94-009-5063-4 |2 doi | |
| 035 | |a (OCoLC)906694325 | ||
| 035 | |a (DE-599)BVBBV042415206 | ||
| 040 | |a DE-604 |b ger |e aacr | ||
| 041 | 0 | |a eng | |
| 049 | |a DE-91 |a DE-83 | ||
| 082 | 0 | |a 531 |2 23 | |
| 084 | |a PHY 000 |2 stub | ||
| 100 | 1 | |a Bushnell, D. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Computerized buckling analysis of shells |c by D. Bushnell |
| 264 | 1 | |a Dordrecht |b Springer Netherlands |c 1989 | |
| 300 | |a 1 Online-Ressource (XVII, 423 p) | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b c |2 rdamedia | ||
| 338 | |b cr |2 rdacarrier | ||
| 490 | 0 | |a Mechanics of Elastic Stability |v 9 |x 0924-2112 | |
| 500 | |a This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways | ||
| 650 | 4 | |a Physics | |
| 650 | 4 | |a Mechanics | |
| 650 | 4 | |a Engineering mathematics | |
| 650 | 4 | |a Appl.Mathematics/Computational Methods of Engineering | |
| 650 | 0 | 7 | |a Elastizitätstheorie |0 (DE-588)4123124-7 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Beulung |0 (DE-588)4145101-6 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Schale |0 (DE-588)4052003-1 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Knickfestigkeit |0 (DE-588)4131084-6 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Schale |0 (DE-588)4052003-1 |D s |
| 689 | 0 | 1 | |a Beulung |0 (DE-588)4145101-6 |D s |
| 689 | 0 | 2 | |a Elastizitätstheorie |0 (DE-588)4123124-7 |D s |
| 689 | 0 | |8 1\p |5 DE-604 | |
| 689 | 1 | 0 | |a Knickfestigkeit |0 (DE-588)4131084-6 |D s |
| 689 | 1 | |8 2\p |5 DE-604 | |
| 856 | 4 | 0 | |u https://doi.org/10.1007/978-94-009-5063-4 |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:BVB01-027850699 | ||
| 883 | 1 | |8 1\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk | |
| 883 | 1 | |8 2\p |a cgwrk |d 20201028 |q DE-101 |u https://d-nb.info/provenance/plan#cgwrk | |
Datensatz im Suchindex
| _version_ | 1804153081943818240 |
|---|---|
| any_adam_object | |
| author | Bushnell, D. |
| author_facet | Bushnell, D. |
| author_role | aut |
| author_sort | Bushnell, D. |
| author_variant | d b db |
| building | Verbundindex |
| bvnumber | BV042415206 |
| classification_tum | PHY 000 |
| collection | ZDB-2-PHA ZDB-2-BAE |
| ctrlnum | (OCoLC)906694325 (DE-599)BVBBV042415206 |
| dewey-full | 531 |
| dewey-hundreds | 500 - Natural sciences and mathematics |
| dewey-ones | 531 - Classical mechanics |
| dewey-raw | 531 |
| dewey-search | 531 |
| dewey-sort | 3531 |
| dewey-tens | 530 - Physics |
| discipline | Physik |
| doi_str_mv | 10.1007/978-94-009-5063-4 |
| format | Electronic eBook |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>03487nmm a2200553zcb4500</leader><controlfield tag="001">BV042415206</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">00000000000000.0</controlfield><controlfield tag="007">cr|uuu---uuuuu</controlfield><controlfield tag="008">150316s1989 |||| o||u| ||||||eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9789400950634</subfield><subfield code="c">Online</subfield><subfield code="9">978-94-009-5063-4</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9789401087414</subfield><subfield code="c">Print</subfield><subfield code="9">978-94-010-8741-4</subfield></datafield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/978-94-009-5063-4</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)906694325</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV042415206</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">531</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">Bushnell, D.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Computerized buckling analysis of shells</subfield><subfield code="c">by D. Bushnell</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Dordrecht</subfield><subfield code="b">Springer Netherlands</subfield><subfield code="c">1989</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 Online-Ressource (XVII, 423 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">Mechanics of Elastic Stability</subfield><subfield code="v">9</subfield><subfield code="x">0924-2112</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Physics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mechanics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Engineering mathematics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Appl.Mathematics/Computational Methods of Engineering</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Elastizitätstheorie</subfield><subfield code="0">(DE-588)4123124-7</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Beulung</subfield><subfield code="0">(DE-588)4145101-6</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Schale</subfield><subfield code="0">(DE-588)4052003-1</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Knickfestigkeit</subfield><subfield code="0">(DE-588)4131084-6</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Schale</subfield><subfield code="0">(DE-588)4052003-1</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="1"><subfield code="a">Beulung</subfield><subfield code="0">(DE-588)4145101-6</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2="2"><subfield code="a">Elastizitätstheorie</subfield><subfield code="0">(DE-588)4123124-7</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="8">1\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="1" ind2="0"><subfield code="a">Knickfestigkeit</subfield><subfield code="0">(DE-588)4131084-6</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2=" "><subfield code="8">2\p</subfield><subfield code="5">DE-604</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://doi.org/10.1007/978-94-009-5063-4</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:BVB01-027850699</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">1\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield><datafield tag="883" ind1="1" ind2=" "><subfield code="8">2\p</subfield><subfield code="a">cgwrk</subfield><subfield code="d">20201028</subfield><subfield code="q">DE-101</subfield><subfield code="u">https://d-nb.info/provenance/plan#cgwrk</subfield></datafield></record></collection> |
| id | DE-604.BV042415206 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T01:20:57Z |
| institution | BVB |
| isbn | 9789400950634 9789401087414 |
| issn | 0924-2112 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-027850699 |
| oclc_num | 906694325 |
| open_access_boolean | |
| owner | DE-91 DE-BY-TUM DE-83 |
| owner_facet | DE-91 DE-BY-TUM DE-83 |
| physical | 1 Online-Ressource (XVII, 423 p) |
| psigel | ZDB-2-PHA ZDB-2-BAE ZDB-2-PHA_Archive |
| publishDate | 1989 |
| publishDateSearch | 1989 |
| publishDateSort | 1989 |
| publisher | Springer Netherlands |
| record_format | marc |
| series2 | Mechanics of Elastic Stability |
| spelling | Bushnell, D. Verfasser aut Computerized buckling analysis of shells by D. Bushnell Dordrecht Springer Netherlands 1989 1 Online-Ressource (XVII, 423 p) txt rdacontent c rdamedia cr rdacarrier Mechanics of Elastic Stability 9 0924-2112 This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways Physics Mechanics Engineering mathematics Appl.Mathematics/Computational Methods of Engineering Elastizitätstheorie (DE-588)4123124-7 gnd rswk-swf Beulung (DE-588)4145101-6 gnd rswk-swf Schale (DE-588)4052003-1 gnd rswk-swf Knickfestigkeit (DE-588)4131084-6 gnd rswk-swf Schale (DE-588)4052003-1 s Beulung (DE-588)4145101-6 s Elastizitätstheorie (DE-588)4123124-7 s 1\p DE-604 Knickfestigkeit (DE-588)4131084-6 s 2\p DE-604 https://doi.org/10.1007/978-94-009-5063-4 Verlag Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 2\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Bushnell, D. Computerized buckling analysis of shells Physics Mechanics Engineering mathematics Appl.Mathematics/Computational Methods of Engineering Elastizitätstheorie (DE-588)4123124-7 gnd Beulung (DE-588)4145101-6 gnd Schale (DE-588)4052003-1 gnd Knickfestigkeit (DE-588)4131084-6 gnd |
| subject_GND | (DE-588)4123124-7 (DE-588)4145101-6 (DE-588)4052003-1 (DE-588)4131084-6 |
| title | Computerized buckling analysis of shells |
| title_auth | Computerized buckling analysis of shells |
| title_exact_search | Computerized buckling analysis of shells |
| title_full | Computerized buckling analysis of shells by D. Bushnell |
| title_fullStr | Computerized buckling analysis of shells by D. Bushnell |
| title_full_unstemmed | Computerized buckling analysis of shells by D. Bushnell |
| title_short | Computerized buckling analysis of shells |
| title_sort | computerized buckling analysis of shells |
| topic | Physics Mechanics Engineering mathematics Appl.Mathematics/Computational Methods of Engineering Elastizitätstheorie (DE-588)4123124-7 gnd Beulung (DE-588)4145101-6 gnd Schale (DE-588)4052003-1 gnd Knickfestigkeit (DE-588)4131084-6 gnd |
| topic_facet | Physics Mechanics Engineering mathematics Appl.Mathematics/Computational Methods of Engineering Elastizitätstheorie Beulung Schale Knickfestigkeit |
| url | https://doi.org/10.1007/978-94-009-5063-4 |
| work_keys_str_mv | AT bushnelld computerizedbucklinganalysisofshells |