An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle:
Gespeichert in:
1. Verfasser: | |
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Format: | Abschlussarbeit Buch |
Sprache: | English |
Veröffentlicht: |
Otaniemi
1975
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Schriftenreihe: | Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja.
52 |
Schlagworte: | |
Beschreibung: | 115 S. graph. Darst. |
Internformat
MARC
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100 | 1 | |a Mai, H. U. |e Verfasser |4 aut | |
245 | 1 | 0 | |a An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
264 | 1 | |a Otaniemi |c 1975 | |
300 | |a 115 S. |b graph. Darst. | ||
336 | |b txt |2 rdacontent | ||
337 | |b n |2 rdamedia | ||
338 | |b nc |2 rdacarrier | ||
490 | 1 | |a Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja. |v 52 | |
502 | |a Zugl.: Helsinki, Univ., Diss., 1975 | ||
650 | 4 | |a Aeroelasticity | |
650 | 4 | |a Mathematical analysis | |
650 | 4 | |a Vortex-motion | |
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830 | 0 | |a Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja. |v 52 |w (DE-604)BV024849179 |9 52 | |
999 | |a oai:aleph.bib-bvb.de:BVB01-001376125 |
Datensatz im Suchindex
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any_adam_object | |
author | Mai, H. U. |
author_facet | Mai, H. U. |
author_role | aut |
author_sort | Mai, H. U. |
author_variant | h u m hu hum |
building | Verbundindex |
bvnumber | BV002099321 |
ctrlnum | (OCoLC)4017149 (DE-599)BVBBV002099321 |
dewey-full | 629.132362 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.132362 |
dewey-search | 629.132362 |
dewey-sort | 3629.132362 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Verkehr / Transport |
format | Thesis Book |
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genre_facet | Hochschulschrift |
id | DE-604.BV002099321 |
illustrated | Illustrated |
indexdate | 2024-07-09T15:40:19Z |
institution | BVB |
language | English |
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series | Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja. |
series2 | Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja. |
spelling | Mai, H. U. Verfasser aut An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle Otaniemi 1975 115 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja. 52 Zugl.: Helsinki, Univ., Diss., 1975 Aeroelasticity Mathematical analysis Vortex-motion (DE-588)4113937-9 Hochschulschrift gnd-content Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja. 52 (DE-604)BV024849179 52 |
spellingShingle | Mai, H. U. An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle Teknillinen Korkeakoulu <Helsinki>: Tieteellisiä julkaisuja. Aeroelasticity Mathematical analysis Vortex-motion |
subject_GND | (DE-588)4113937-9 |
title | An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
title_auth | An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
title_exact_search | An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
title_full | An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
title_fullStr | An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
title_full_unstemmed | An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
title_short | An unsteady Vortex panel method and its application to arroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
title_sort | an unsteady vortex panel method and its application to arroelastic calculations of a fixed thin wing and an unconstrained flying vehicle |
topic | Aeroelasticity Mathematical analysis Vortex-motion |
topic_facet | Aeroelasticity Mathematical analysis Vortex-motion Hochschulschrift |
volume_link | (DE-604)BV024849179 |
work_keys_str_mv | AT maihu anunsteadyvortexpanelmethodanditsapplicationtoarroelasticcalculationsofafixedthinwingandanunconstrainedflyingvehicle |