Advanced method for computing the flow around wings with rear separation and ground effect:
Gespeichert in:
| Beteilige Person: | |
|---|---|
| Format: | Buch |
| Sprache: | Englisch |
| Veröffentlicht: |
Köln
1986
|
| Schriftenreihe: | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht
1986,17 |
| Schlagwörter: | |
| Umfang: | 62 S. Ill., graph. Darst. |
Internformat
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| 490 | 1 | |a Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |v 1986,17 | |
| 650 | 7 | |a Grenzschichtablösung |2 swd | |
| 650 | 7 | |a Tragflügel |2 swd | |
| 650 | 4 | |a Mathematisches Modell | |
| 650 | 4 | |a Aerodynamics |x Mathematical models | |
| 650 | 4 | |a Airplanes |x Wings | |
| 650 | 4 | |a Ground-cushion phenomena | |
| 650 | 0 | 7 | |a Unterschallströmung |0 (DE-588)4135418-7 |2 gnd |9 rswk-swf |
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Datensatz im Suchindex
| DE-BY-TUM_call_number | 0701 96 A 1634-1986,17 |
|---|---|
| DE-BY-TUM_katkey | 875615 |
| DE-BY-TUM_location | Mag |
| DE-BY-TUM_media_number | 040070213126 |
| _version_ | 1821931236753408001 |
| any_adam_object | |
| author | Jacob, Klaus |
| author_facet | Jacob, Klaus |
| author_role | aut |
| author_sort | Jacob, Klaus |
| author_variant | k j kj |
| building | Verbundindex |
| bvnumber | BV000512589 |
| callnumber-first | T - Technology |
| callnumber-label | TL574 |
| callnumber-raw | TL574.F5 |
| callnumber-search | TL574.F5 |
| callnumber-sort | TL 3574 F5 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| ctrlnum | (OCoLC)15747970 (DE-599)BVBBV000512589 |
| format | Book |
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| id | DE-604.BV000512589 |
| illustrated | Illustrated |
| indexdate | 2024-12-20T07:22:12Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-000316639 |
| oclc_num | 15747970 |
| open_access_boolean | |
| owner | DE-12 DE-91G DE-BY-TUM DE-210 DE-M122 |
| owner_facet | DE-12 DE-91G DE-BY-TUM DE-210 DE-M122 |
| physical | 62 S. Ill., graph. Darst. |
| publishDate | 1986 |
| publishDateSearch | 1986 |
| publishDateSort | 1986 |
| record_format | marc |
| series | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |
| series2 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht |
| spellingShingle | Jacob, Klaus Advanced method for computing the flow around wings with rear separation and ground effect Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt <Köln>: Forschungsbericht Grenzschichtablösung swd Tragflügel swd Mathematisches Modell Aerodynamics Mathematical models Airplanes Wings Ground-cushion phenomena 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_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 | Grenzschichtablösung swd Tragflügel swd Mathematisches Modell Aerodynamics Mathematical models Airplanes Wings Ground-cushion phenomena Unterschallströmung (DE-588)4135418-7 gnd Grenzschichtablösung (DE-588)4136915-4 gnd Tragflügel (DE-588)4060582-6 gnd |
| topic_facet | Grenzschichtablösung Tragflügel Mathematisches Modell Aerodynamics Mathematical models Airplanes Wings Ground-cushion phenomena Unterschallströmung |
| volume_link | (DE-604)BV011052093 |
| work_keys_str_mv | AT jacobklaus advancedmethodforcomputingtheflowaroundwingswithrearseparationandgroundeffect |
Paper/Kapitel scannen lassen
Bibliotheksmagazin
| Signatur: |
0701 96 A 1634-1986,17 Lageplan |
|---|---|
| Exemplar 1 | Ausleihbar Am Standort |