Verfügbarkeit: Wing theory in supersonic flow

Wing theory in supersonic flow:

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Bibliographische Detailangaben
1. Verfasser:	Carafoli, Elie (VerfasserIn)
Format:	Elektronisch E-Book
Sprache:	English
Veröffentlicht:	Oxford Pergamon Press [1969]
Ausgabe:	[1st ed.]
Schriftenreihe:	International series of monographs in aeronautics and astronautics v. 7
Schlagworte:	Aerodynamics, Supersonic Airplanes / Wings TECHNOLOGY & ENGINEERING / Engineering (General) Airplanes > Wings Deltaflügel Überschallströmung Berechnung Bemessungsgrundlage
Online-Zugang:	FAW01 Volltext
Beschreibung:	Includes bibliographical references (pages 565-588) Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the
Beschreibung:	xiii, 594 pages
ISBN:	9781483160276 1483160270 0080123309 9780080123301

Internformat

MARC


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Datensatz im Suchindex

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any_adam_object
author	Carafoli, Elie
author_facet	Carafoli, Elie
author_role	aut
author_sort	Carafoli, Elie
author_variant	e c ec
building	Verbundindex
bvnumber	BV044386275
collection	ZDB-33-ESD
ctrlnum	(ZDB-33-ESD)ocn608848090 (OCoLC)608848090 (DE-599)BVBBV044386275
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
edition	[1st ed.]
format	Electronic eBook
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id	DE-604.BV044386275
illustrated	Not Illustrated
indexdate	2024-07-10T07:51:30Z
institution	BVB
isbn	9781483160276 1483160270 0080123309 9780080123301
language	English
oai_aleph_id	oai:aleph.bib-bvb.de:BVB01-029788496
oclc_num	608848090
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owner	DE-1046
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physical	xiii, 594 pages
psigel	ZDB-33-ESD ZDB-33-ESD FAW_PDA_ESD
publishDate	1969
publishDateSearch	1969
publishDateSort	1969
publisher	Pergamon Press
record_format	marc
series2	International series of monographs in aeronautics and astronautics
spelling	Carafoli, Elie Verfasser aut Wing theory in supersonic flow by Elie Carafoli ; with the cooperation of Dan Mateescu and Adriana Nastase [1st ed.] Oxford Pergamon Press [1969] xiii, 594 pages txt rdacontent c rdamedia cr rdacarrier International series of monographs in aeronautics and astronautics v. 7 Includes bibliographical references (pages 565-588) Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the Aerodynamics, Supersonic fast Airplanes / Wings fast TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Aerodynamics, Supersonic Airplanes Wings Deltaflügel (DE-588)4200520-6 gnd rswk-swf Überschallströmung (DE-588)4186626-5 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 1\p DE-604 Bemessungsgrundlage (DE-588)4133748-7 s 2\p DE-604 Deltaflügel (DE-588)4200520-6 s 3\p DE-604 Überschallströmung (DE-588)4186626-5 s 4\p DE-604 Mateescu, Dan Sonstige oth Năstase, Adriana Sonstige oth http://www.sciencedirect.com/science/book/9780080123301 Verlag URL des Erstveröffentlichers Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 2\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 3\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 4\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk
spellingShingle	Carafoli, Elie Wing theory in supersonic flow Aerodynamics, Supersonic fast Airplanes / Wings fast TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Aerodynamics, Supersonic Airplanes Wings Deltaflügel (DE-588)4200520-6 gnd Überschallströmung (DE-588)4186626-5 gnd Berechnung (DE-588)4120997-7 gnd Bemessungsgrundlage (DE-588)4133748-7 gnd
subject_GND	(DE-588)4200520-6 (DE-588)4186626-5 (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_full	Wing theory in supersonic flow by Elie Carafoli ; with the cooperation of Dan Mateescu and Adriana Nastase
title_fullStr	Wing theory in supersonic flow by Elie Carafoli ; with the cooperation of Dan Mateescu and Adriana Nastase
title_full_unstemmed	Wing theory in supersonic flow by Elie Carafoli ; with the cooperation of Dan Mateescu and Adriana Nastase
title_short	Wing theory in supersonic flow
title_sort	wing theory in supersonic flow
topic	Aerodynamics, Supersonic fast Airplanes / Wings fast TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Aerodynamics, Supersonic Airplanes Wings Deltaflügel (DE-588)4200520-6 gnd Überschallströmung (DE-588)4186626-5 gnd Berechnung (DE-588)4120997-7 gnd Bemessungsgrundlage (DE-588)4133748-7 gnd
topic_facet	Aerodynamics, Supersonic Airplanes / Wings TECHNOLOGY & ENGINEERING / Engineering (General) Airplanes Wings Deltaflügel Überschallströmung Berechnung Bemessungsgrundlage
url	http://www.sciencedirect.com/science/book/9780080123301
work_keys_str_mv	AT carafolielie wingtheoryinsupersonicflow AT mateescudan wingtheoryinsupersonicflow AT nastaseadriana wingtheoryinsupersonicflow

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