The strength of shell bodies-- theory and practice:
The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell s...
Gespeichert in:
1. Verfasser: | |
---|---|
Format: | Elektronisch E-Book |
Sprache: | English |
Veröffentlicht: |
Washington, D.C
National Advisory Commitee for Aeronautics
1937
|
Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Technical memorandum
838 |
Schlagworte: | |
Online-Zugang: | Volltext |
Zusammenfassung: | The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject |
Beschreibung: | "September 1937. - Includes bibliographical references. - NACA TM No. 838. - Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics |
Beschreibung: | 1 Online-Ressource (51 p., 9 unnumbered pages) |
ISBN: | 9781680156560 |
Internformat
MARC
LEADER | 00000nmm a2200000 cb4500 | ||
---|---|---|---|
001 | BV043976651 | ||
003 | DE-604 | ||
007 | cr|uuu---uuuuu | ||
008 | 161222s1937 |||| o||u| ||||||eng d | ||
020 | |a 9781680156560 |c Online |9 978-1-68015-656-0 | ||
035 | |a (OCoLC)968690335 | ||
035 | |a (DE-599)GBV856592366 | ||
040 | |a DE-604 |b ger |e rda | ||
041 | 0 | |a eng | |
050 | 0 | |a TA660.S5 | |
082 | 0 | |a 624.17762 | |
100 | 1 | |a Ebner, H. |e Verfasser |4 aut | |
245 | 1 | 0 | |a The strength of shell bodies-- theory and practice |c H. Ebner |
264 | 1 | |a Washington, D.C |b National Advisory Commitee for Aeronautics |c 1937 | |
300 | |a 1 Online-Ressource (51 p., 9 unnumbered pages) | ||
336 | |b txt |2 rdacontent | ||
337 | |b c |2 rdamedia | ||
338 | |b cr |2 rdacarrier | ||
490 | 1 | |a United States / National Advisory Committee for Aeronautics: Technical memorandum |v 838 | |
500 | |a "September 1937. - Includes bibliographical references. - NACA TM No. 838. - Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics | ||
520 | 8 | |a The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject | |
650 | 4 | |a Mathematik | |
650 | 4 | |a Monocoque construction | |
650 | 4 | |a Mathematics | |
650 | 4 | |a Strains and stresses | |
650 | 4 | |a Shells (Engineering) | |
810 | 2 | |a National Advisory Committee for Aeronautics: Technical memorandum |t United States |v 838 |w (DE-604)BV008909669 |9 838 | |
856 | 4 | 0 | |u http://app.knovel.com/hotlink/toc/id:kpSSBTPNA1/strength_of_shell_bodies__theory_and_practice_naca_technical_memorandums_838 |x Aggregator |3 Volltext |
912 | |a ZDB-10-KNL |a ZDB-10-ARA | ||
943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-029385126 |
Datensatz im Suchindex
_version_ | 1806054961016995840 |
---|---|
adam_text | |
any_adam_object | |
author | Ebner, H. |
author_facet | Ebner, H. |
author_role | aut |
author_sort | Ebner, H. |
author_variant | h e he |
building | Verbundindex |
bvnumber | BV043976651 |
callnumber-first | T - Technology |
callnumber-label | TA660 |
callnumber-raw | TA660.S5 |
callnumber-search | TA660.S5 |
callnumber-sort | TA 3660 S5 |
callnumber-subject | TA - General and Civil Engineering |
collection | ZDB-10-KNL ZDB-10-ARA |
ctrlnum | (OCoLC)968690335 (DE-599)GBV856592366 |
dewey-full | 624.17762 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 624 - Civil engineering |
dewey-raw | 624.17762 |
dewey-search | 624.17762 |
dewey-sort | 3624.17762 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Bauingenieurwesen |
format | Electronic eBook |
fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>00000nmm a2200000 cb4500</leader><controlfield tag="001">BV043976651</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="007">cr|uuu---uuuuu</controlfield><controlfield tag="008">161222s1937 |||| o||u| ||||||eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9781680156560</subfield><subfield code="c">Online</subfield><subfield code="9">978-1-68015-656-0</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)968690335</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)GBV856592366</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield><subfield code="e">rda</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="050" ind1=" " ind2="0"><subfield code="a">TA660.S5</subfield></datafield><datafield tag="082" ind1="0" ind2=" "><subfield code="a">624.17762</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Ebner, H.</subfield><subfield code="e">Verfasser</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">The strength of shell bodies-- theory and practice</subfield><subfield code="c">H. Ebner</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Washington, D.C</subfield><subfield code="b">National Advisory Commitee for Aeronautics</subfield><subfield code="c">1937</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 Online-Ressource (51 p., 9 unnumbered pages)</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="1" ind2=" "><subfield code="a">United States / National Advisory Committee for Aeronautics: Technical memorandum</subfield><subfield code="v">838</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">"September 1937. - Includes bibliographical references. - NACA TM No. 838. - Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics</subfield></datafield><datafield tag="520" ind1="8" ind2=" "><subfield code="a">The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mathematik</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Monocoque construction</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Mathematics</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Strains and stresses</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Shells (Engineering)</subfield></datafield><datafield tag="810" ind1="2" ind2=" "><subfield code="a">National Advisory Committee for Aeronautics: Technical memorandum</subfield><subfield code="t">United States</subfield><subfield code="v">838</subfield><subfield code="w">(DE-604)BV008909669</subfield><subfield code="9">838</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">http://app.knovel.com/hotlink/toc/id:kpSSBTPNA1/strength_of_shell_bodies__theory_and_practice_naca_technical_memorandums_838</subfield><subfield code="x">Aggregator</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">ZDB-10-KNL</subfield><subfield code="a">ZDB-10-ARA</subfield></datafield><datafield tag="943" ind1="1" ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-029385126</subfield></datafield></record></collection> |
id | DE-604.BV043976651 |
illustrated | Not Illustrated |
indexdate | 2024-07-31T01:10:29Z |
institution | BVB |
isbn | 9781680156560 |
language | English |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029385126 |
oclc_num | 968690335 |
open_access_boolean | |
owner | DE-91 DE-BY-TUM |
owner_facet | DE-91 DE-BY-TUM |
physical | 1 Online-Ressource (51 p., 9 unnumbered pages) |
psigel | ZDB-10-KNL ZDB-10-ARA |
publishDate | 1937 |
publishDateSearch | 1937 |
publishDateSort | 1937 |
publisher | National Advisory Commitee for Aeronautics |
record_format | marc |
series2 | United States / National Advisory Committee for Aeronautics: Technical memorandum |
spelling | Ebner, H. Verfasser aut The strength of shell bodies-- theory and practice H. Ebner Washington, D.C National Advisory Commitee for Aeronautics 1937 1 Online-Ressource (51 p., 9 unnumbered pages) txt rdacontent c rdamedia cr rdacarrier United States / National Advisory Committee for Aeronautics: Technical memorandum 838 "September 1937. - Includes bibliographical references. - NACA TM No. 838. - Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject Mathematik Monocoque construction Mathematics Strains and stresses Shells (Engineering) National Advisory Committee for Aeronautics: Technical memorandum United States 838 (DE-604)BV008909669 838 http://app.knovel.com/hotlink/toc/id:kpSSBTPNA1/strength_of_shell_bodies__theory_and_practice_naca_technical_memorandums_838 Aggregator Volltext |
spellingShingle | Ebner, H. The strength of shell bodies-- theory and practice Mathematik Monocoque construction Mathematics Strains and stresses Shells (Engineering) |
title | The strength of shell bodies-- theory and practice |
title_auth | The strength of shell bodies-- theory and practice |
title_exact_search | The strength of shell bodies-- theory and practice |
title_full | The strength of shell bodies-- theory and practice H. Ebner |
title_fullStr | The strength of shell bodies-- theory and practice H. Ebner |
title_full_unstemmed | The strength of shell bodies-- theory and practice H. Ebner |
title_short | The strength of shell bodies-- theory and practice |
title_sort | the strength of shell bodies theory and practice |
topic | Mathematik Monocoque construction Mathematics Strains and stresses Shells (Engineering) |
topic_facet | Mathematik Monocoque construction Mathematics Strains and stresses Shells (Engineering) |
url | http://app.knovel.com/hotlink/toc/id:kpSSBTPNA1/strength_of_shell_bodies__theory_and_practice_naca_technical_memorandums_838 |
volume_link | (DE-604)BV008909669 |
work_keys_str_mv | AT ebnerh thestrengthofshellbodiestheoryandpractice |