Theory of aerospace propulsion:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Amsterdam
Elsevier Butterworth-Heinemann
[2017]
|
| Ausgabe: | Second edition |
| Schriftenreihe: | Aeronautical engineering
|
| Schlagworte: | |
| Online-Zugang: | BTU01 FAW01 FLA01 Volltext |
| Beschreibung: | Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components. Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance. Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration Includes bibliographical references and index |
| Beschreibung: | 1 Online-Ressource (xx, 827 Seiten) Illustrationen, Diagramme |
| ISBN: | 9780128093269 |
Internformat
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| 245 | 1 | 0 | |a Theory of aerospace propulsion |c Pasquale M. Sforza, University of Florida |
| 250 | |a Second edition | ||
| 264 | 1 | |a Amsterdam |b Elsevier Butterworth-Heinemann |c [2017] | |
| 264 | 4 | |c © 2017 | |
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| 338 | |b cr |2 rdacarrier | ||
| 490 | 0 | |a Aeronautical engineering | |
| 500 | |a Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components. Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance. Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration | ||
| 500 | |a Includes bibliographical references and index | ||
| 650 | 7 | |a Jet propulsion |2 fast | |
| 650 | 4 | |a Jet propulsion | |
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Datensatz im Suchindex
| _version_ | 1804177648573743104 |
|---|---|
| any_adam_object | |
| author | Sforza, Pasquale M. |
| author_facet | Sforza, Pasquale M. |
| author_role | aut |
| author_sort | Sforza, Pasquale M. |
| author_variant | p m s pm pms |
| building | Verbundindex |
| bvnumber | BV044383415 |
| classification_rvk | ZO 7275 |
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| ctrlnum | (ZDB-33-ESD)ocn858453380 (OCoLC)858453380 (DE-599)BVBBV044383415 |
| dewey-full | 629.1/1 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.1/1 |
| dewey-search | 629.1/1 |
| dewey-sort | 3629.1 11 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| edition | Second edition |
| format | Electronic eBook |
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| id | DE-604.BV044383415 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T07:51:25Z |
| institution | BVB |
| isbn | 9780128093269 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029785636 |
| oclc_num | 858453380 |
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| physical | 1 Online-Ressource (xx, 827 Seiten) Illustrationen, Diagramme |
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| publishDate | 2017 |
| publishDateSearch | 2017 |
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| publisher | Elsevier Butterworth-Heinemann |
| record_format | marc |
| series2 | Aeronautical engineering |
| spelling | Sforza, Pasquale M. Verfasser aut Theory of aerospace propulsion Pasquale M. Sforza, University of Florida Second edition Amsterdam Elsevier Butterworth-Heinemann [2017] © 2017 1 Online-Ressource (xx, 827 Seiten) Illustrationen, Diagramme txt rdacontent c rdamedia cr rdacarrier Aeronautical engineering Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components. Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance. Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration Includes bibliographical references and index Jet propulsion fast Jet propulsion Luftstrahltriebwerk (DE-588)4128278-4 gnd rswk-swf Raketentriebwerk (DE-588)4176905-3 gnd rswk-swf Flugtriebwerk (DE-588)4154773-1 gnd rswk-swf Luftstrahltriebwerk (DE-588)4128278-4 s DE-604 Raketentriebwerk (DE-588)4176905-3 s 1\p DE-604 Flugtriebwerk (DE-588)4154773-1 s 2\p DE-604 Erscheint auch als Druck-Ausgabe 978-0-12-809326-9 http://www.sciencedirect.com/science/book/9780128093269 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 |
| spellingShingle | Sforza, Pasquale M. Theory of aerospace propulsion Jet propulsion fast Jet propulsion Luftstrahltriebwerk (DE-588)4128278-4 gnd Raketentriebwerk (DE-588)4176905-3 gnd Flugtriebwerk (DE-588)4154773-1 gnd |
| subject_GND | (DE-588)4128278-4 (DE-588)4176905-3 (DE-588)4154773-1 |
| title | Theory of aerospace propulsion |
| title_auth | Theory of aerospace propulsion |
| title_exact_search | Theory of aerospace propulsion |
| title_full | Theory of aerospace propulsion Pasquale M. Sforza, University of Florida |
| title_fullStr | Theory of aerospace propulsion Pasquale M. Sforza, University of Florida |
| title_full_unstemmed | Theory of aerospace propulsion Pasquale M. Sforza, University of Florida |
| title_short | Theory of aerospace propulsion |
| title_sort | theory of aerospace propulsion |
| topic | Jet propulsion fast Jet propulsion Luftstrahltriebwerk (DE-588)4128278-4 gnd Raketentriebwerk (DE-588)4176905-3 gnd Flugtriebwerk (DE-588)4154773-1 gnd |
| topic_facet | Jet propulsion Luftstrahltriebwerk Raketentriebwerk Flugtriebwerk |
| url | http://www.sciencedirect.com/science/book/9780128093269 |
| work_keys_str_mv | AT sforzapasqualem theoryofaerospacepropulsion |