Advanced method for computing the flow around wings with rear separation and ground effect:
Gespeichert in:
1. Verfasser: | |
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Format: | Buch |
Sprache: | German |
Veröffentlicht: |
Köln
Wiss. Berichtswesen der DFVLR
1986
|
Ausgabe: | Als Ms. gedr. |
Schriftenreihe: | Forschungsbericht / Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt
86-17 |
Schlagworte: | |
Beschreibung: | 62 S. graph. Darst. |
Internformat
MARC
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Datensatz im Suchindex
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author | Jacob, Klaus |
author_facet | Jacob, Klaus |
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author_sort | Jacob, Klaus |
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id | DE-604.BV022050584 |
illustrated | Illustrated |
index_date | 2024-07-02T16:13:18Z |
indexdate | 2024-07-09T20:49:51Z |
institution | BVB |
language | German |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-015265308 |
oclc_num | 74784118 |
open_access_boolean | |
owner | DE-706 |
owner_facet | DE-706 |
physical | 62 S. graph. Darst. |
publishDate | 1986 |
publishDateSearch | 1986 |
publishDateSort | 1986 |
publisher | Wiss. Berichtswesen der DFVLR |
record_format | marc |
series2 | Forschungsbericht / Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt |
spelling | Jacob, Klaus Verfasser aut Advanced method for computing the flow around wings with rear separation and ground effect Als Ms. gedr. Köln Wiss. Berichtswesen der DFVLR 1986 62 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Forschungsbericht / Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt 86-17 Unterschallströmung (DE-588)4135418-7 gnd rswk-swf Grenzschichtablösung (DE-588)4136915-4 gnd rswk-swf Tragflügel (DE-588)4060582-6 gnd rswk-swf Unterschallströmung (DE-588)4135418-7 s DE-604 Tragflügel (DE-588)4060582-6 s Grenzschichtablösung (DE-588)4136915-4 s 1\p DE-604 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt Forschungsbericht 86-17 (DE-604)BV011052093 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
spellingShingle | Jacob, Klaus Advanced method for computing the flow around wings with rear separation and ground effect Unterschallströmung (DE-588)4135418-7 gnd Grenzschichtablösung (DE-588)4136915-4 gnd Tragflügel (DE-588)4060582-6 gnd |
subject_GND | (DE-588)4135418-7 (DE-588)4136915-4 (DE-588)4060582-6 |
title | Advanced method for computing the flow around wings with rear separation and ground effect |
title_auth | Advanced method for computing the flow around wings with rear separation and ground effect |
title_exact_search | Advanced method for computing the flow around wings with rear separation and ground effect |
title_exact_search_txtP | Advanced method for computing the flow around wings with rear separation and ground effect |
title_full | Advanced method for computing the flow around wings with rear separation and ground effect |
title_fullStr | Advanced method for computing the flow around wings with rear separation and ground effect |
title_full_unstemmed | Advanced method for computing the flow around wings with rear separation and ground effect |
title_short | Advanced method for computing the flow around wings with rear separation and ground effect |
title_sort | advanced method for computing the flow around wings with rear separation and ground effect |
topic | Unterschallströmung (DE-588)4135418-7 gnd Grenzschichtablösung (DE-588)4136915-4 gnd Tragflügel (DE-588)4060582-6 gnd |
topic_facet | Unterschallströmung Grenzschichtablösung Tragflügel |
volume_link | (DE-604)BV011052093 |
work_keys_str_mv | AT jacobklaus advancedmethodforcomputingtheflowaroundwingswithrearseparationandgroundeffect |