An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Abschlussarbeit Buch |
| Sprache: | English |
| Veröffentlicht: |
Otaniemi
1975
|
| Schriftenreihe: | Helsingin Teknillinen Korkeakoulu tieteellisiae julkaisuja
52 |
| Schlagworte: | |
| Beschreibung: | 115 S. |
Internformat
MARC
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Datensatz im Suchindex
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| author | Mai, H Ulv |
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| id | DE-604.BV024851692 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-09T22:22:26Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-019528148 |
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| owner_facet | DE-11 |
| physical | 115 S. |
| publishDate | 1975 |
| publishDateSearch | 1975 |
| publishDateSort | 1975 |
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| series2 | Helsingin Teknillinen Korkeakoulu tieteellisiae julkaisuja |
| spelling | Mai, H Ulv Verfasser aut An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle H. Ulv Mai Otaniemi 1975 115 S. txt rdacontent n rdamedia nc rdacarrier Helsingin Teknillinen Korkeakoulu tieteellisiae julkaisuja 52 Zugl.: Helsinki, Univ., Diss., 1975 (DE-588)4113937-9 Hochschulschrift gnd-content Teknillinen Korkeakoulu <Helsinki> Helsingin Teknillinen Korkeakoulu tieteellisiae julkaisuja 52 (DE-604)BV024849179 52 |
| spellingShingle | Mai, H Ulv An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
| subject_GND | (DE-588)4113937-9 |
| title | An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
| title_auth | An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
| title_exact_search | An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
| title_full | An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle H. Ulv Mai |
| title_fullStr | An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle H. Ulv Mai |
| title_full_unstemmed | An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle H. Ulv Mai |
| title_short | An unsteady vortex panel method and its application to aeroelastic calculations of a fixed, thin wing and an unconstrained flying vehicle |
| title_sort | an unsteady vortex panel method and its application to aeroelastic calculations of a fixed thin wing and an unconstrained flying vehicle |
| topic_facet | Hochschulschrift |
| volume_link | (DE-604)BV024849179 |
| work_keys_str_mv | AT maihulv anunsteadyvortexpanelmethodanditsapplicationtoaeroelasticcalculationsofafixedthinwingandanunconstrainedflyingvehicle |