Wing theory in supersonic flow:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Oxford [u.a.]
Pergamon Press
1969
|
| Ausgabe: | 1. ed. |
| Schriftenreihe: | International series of monographs in aeronautics and astronautics
Division 2, Aerodynamics ; 7 |
| Schlagworte: | |
| Beschreibung: | Literaturverz. S. 565 - 588 |
| Beschreibung: | XIII, 594 S. graph. Darst. |
| ISBN: | 0080123309 |
Internformat
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| 245 | 1 | 0 | |a Wing theory in supersonic flow |c by Elie Carafoli |
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| 264 | 1 | |a Oxford [u.a.] |b Pergamon Press |c 1969 | |
| 300 | |a XIII, 594 S. |b graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
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| 490 | 1 | |a International series of monographs in aeronautics and astronautics : Division 2, Aerodynamics |v 7 | |
| 500 | |a Literaturverz. S. 565 - 588 | ||
| 650 | 4 | |a Aerodynamics, Supersonic | |
| 650 | 4 | |a Airplanes |x Wings | |
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Datensatz im Suchindex
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| author | Carafoli, Elie |
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| bvnumber | BV022155570 |
| callnumber-first | T - Technology |
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| callnumber-raw | TL672 |
| callnumber-search | TL672 |
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| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | ZO 7230 |
| ctrlnum | (OCoLC)180754 (DE-599)BVBBV022155570 |
| dewey-full | 629.13432 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.13432 |
| dewey-search | 629.13432 |
| dewey-sort | 3629.13432 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| discipline_str_mv | Verkehr / Transport |
| edition | 1. ed. |
| format | Book |
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| id | DE-604.BV022155570 |
| illustrated | Illustrated |
| index_date | 2024-07-02T16:18:28Z |
| indexdate | 2024-07-09T20:51:30Z |
| institution | BVB |
| isbn | 0080123309 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-015370229 |
| oclc_num | 180754 |
| open_access_boolean | |
| owner | DE-706 DE-188 |
| owner_facet | DE-706 DE-188 |
| physical | XIII, 594 S. graph. Darst. |
| publishDate | 1969 |
| publishDateSearch | 1969 |
| publishDateSort | 1969 |
| publisher | Pergamon Press |
| record_format | marc |
| series | International series of monographs in aeronautics and astronautics |
| series2 | International series of monographs in aeronautics and astronautics : Division 2, Aerodynamics |
| spelling | Carafoli, Elie Verfasser (DE-588)126267626 aut Wing theory in supersonic flow by Elie Carafoli 1. ed. Oxford [u.a.] Pergamon Press 1969 XIII, 594 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier International series of monographs in aeronautics and astronautics : Division 2, Aerodynamics 7 Literaturverz. S. 565 - 588 Aerodynamics, Supersonic Airplanes Wings Überschallströmung (DE-588)4186626-5 gnd rswk-swf Deltaflügel (DE-588)4200520-6 gnd rswk-swf Berechnung (DE-588)4120997-7 gnd rswk-swf Bemessungsgrundlage (DE-588)4133748-7 gnd rswk-swf Berechnung (DE-588)4120997-7 s DE-604 Bemessungsgrundlage (DE-588)4133748-7 s Überschallströmung (DE-588)4186626-5 s Deltaflügel (DE-588)4200520-6 s International series of monographs in aeronautics and astronautics Division 2, Aerodynamics ; 7 (DE-604)BV004081457 7 |
| spellingShingle | Carafoli, Elie Wing theory in supersonic flow International series of monographs in aeronautics and astronautics Aerodynamics, Supersonic Airplanes Wings Überschallströmung (DE-588)4186626-5 gnd Deltaflügel (DE-588)4200520-6 gnd Berechnung (DE-588)4120997-7 gnd Bemessungsgrundlage (DE-588)4133748-7 gnd |
| subject_GND | (DE-588)4186626-5 (DE-588)4200520-6 (DE-588)4120997-7 (DE-588)4133748-7 |
| title | Wing theory in supersonic flow |
| title_auth | Wing theory in supersonic flow |
| title_exact_search | Wing theory in supersonic flow |
| title_exact_search_txtP | Wing theory in supersonic flow |
| title_full | Wing theory in supersonic flow by Elie Carafoli |
| title_fullStr | Wing theory in supersonic flow by Elie Carafoli |
| title_full_unstemmed | Wing theory in supersonic flow by Elie Carafoli |
| title_short | Wing theory in supersonic flow |
| title_sort | wing theory in supersonic flow |
| topic | Aerodynamics, Supersonic Airplanes Wings Überschallströmung (DE-588)4186626-5 gnd Deltaflügel (DE-588)4200520-6 gnd Berechnung (DE-588)4120997-7 gnd Bemessungsgrundlage (DE-588)4133748-7 gnd |
| topic_facet | Aerodynamics, Supersonic Airplanes Wings Überschallströmung Deltaflügel Berechnung Bemessungsgrundlage |
| volume_link | (DE-604)BV004081457 |
| work_keys_str_mv | AT carafolielie wingtheoryinsupersonicflow |