Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen:
Gespeichert in:
1. Verfasser: | |
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Format: | Elektronisch E-Book |
Sprache: | German |
Veröffentlicht: |
2005
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Schlagworte: | |
Online-Zugang: | kostenfrei https://nbn-resolving.org/urn:nbn:de:bvb:91-diss20051104-1540148180 |
Beschreibung: | München, Techn. Univ., Diss., 2005 |
Beschreibung: | 1 Online-Ressource |
Internformat
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Datensatz im Suchindex
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author | Haryanto, Ismoyo 1966- |
author_GND | (DE-588)130654949 |
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author_variant | i h ih |
building | Verbundindex |
bvnumber | BV021233619 |
classification_tum | MAS 036d VER 605d |
collection | ebook |
ctrlnum | (OCoLC)615000694 (DE-599)BVBBV021233619 |
dewey-full | 629.134320151825 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.134320151825 |
dewey-search | 629.134320151825 |
dewey-sort | 3629.134320151825 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Verkehrstechnik Verkehr / Transport Maschinenbau |
discipline_str_mv | Verkehrstechnik Verkehr / Transport Maschinenbau |
format | Electronic eBook |
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spelling | Haryanto, Ismoyo 1966- Verfasser (DE-588)130654949 aut Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen Ismoyo Haryanto 2005 1 Online-Ressource txt rdacontent c rdamedia cr rdacarrier München, Techn. Univ., Diss., 2005 Tragflügel (DE-588)4060582-6 gnd rswk-swf Strukturoptimierung (DE-588)4183811-7 gnd rswk-swf Finite-Elemente-Methode (DE-588)4017233-8 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Tragflügel (DE-588)4060582-6 s Strukturoptimierung (DE-588)4183811-7 s Finite-Elemente-Methode (DE-588)4017233-8 s DE-604 ca. 0,9 MB http://mediatum.ub.tum.de/?id=601951 Verlag kostenfrei https://nbn-resolving.org/urn:nbn:de:bvb:91-diss20051104-1540148180 Resolving-System |
spellingShingle | Haryanto, Ismoyo 1966- Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen Tragflügel (DE-588)4060582-6 gnd Strukturoptimierung (DE-588)4183811-7 gnd Finite-Elemente-Methode (DE-588)4017233-8 gnd |
subject_GND | (DE-588)4060582-6 (DE-588)4183811-7 (DE-588)4017233-8 (DE-588)4113937-9 |
title | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen |
title_auth | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen |
title_exact_search | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen |
title_exact_search_txtP | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen |
title_full | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen Ismoyo Haryanto |
title_fullStr | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen Ismoyo Haryanto |
title_full_unstemmed | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen Ismoyo Haryanto |
title_short | Aeroelastische Optimierung von Tragflügelstrukturen mit semi-analytischen Finite-Element-Modellen |
title_sort | aeroelastische optimierung von tragflugelstrukturen mit semi analytischen finite element modellen |
topic | Tragflügel (DE-588)4060582-6 gnd Strukturoptimierung (DE-588)4183811-7 gnd Finite-Elemente-Methode (DE-588)4017233-8 gnd |
topic_facet | Tragflügel Strukturoptimierung Finite-Elemente-Methode Hochschulschrift |
url | http://mediatum.ub.tum.de/?id=601951 https://nbn-resolving.org/urn:nbn:de:bvb:91-diss20051104-1540148180 |
work_keys_str_mv | AT haryantoismoyo aeroelastischeoptimierungvontragflugelstrukturenmitsemianalytischenfiniteelementmodellen |