Performance and stability of aircraft:
Gespeichert in:
1. Verfasser: | |
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Format: | Elektronisch E-Book |
Sprache: | English |
Veröffentlicht: |
London
Arnold
1996
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Schlagworte: | |
Online-Zugang: | Volltext |
Beschreibung: | The performance, stability, control and response of aircraft are key areas of aeronautical engineering. This book provides a comprehensive overview to the underlying theory and application of what are often perceived to be difficult topics. Initially it introduces the reader to the fundamental concepts underlying performance and stability, including lift characteristics and estimation of drag, before moving on to a more detailed analysis of performance in both level and climbing flight. Pitching motion is then described followed by a detailed discussion of all aspects of both lateral and longitudinal stability and response. It finishes with an examination of inertial cross-coupling and automatic control and stabilization. The student is helped to think in three dimensions throughout the book by the use of illustrative examples. The progression from one degree of freedom to six degrees of freedom is gradually introduced. The result is an approach dealing specifically with all aspects of performance, stability and control that fills a gap in the current literature. It will be essential reading for all those embarking on degree level courses in aeronautical engineering and will be of interest to all with an interest in stability and dynamics, including those in commercial flying schools who require an insight into the performance of their aircraft. Ideal for undergraduate aeronautical engineers Three-dimensional thinking introduced through worked examples and simple situations Includes bibliographical references (p. [285-286]) and index |
Beschreibung: | 1 Online-Ressource (xx, 294) |
ISBN: | 9780340631706 0340631708 0080538649 9780080538648 0470235985 |
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500 | |a The performance, stability, control and response of aircraft are key areas of aeronautical engineering. This book provides a comprehensive overview to the underlying theory and application of what are often perceived to be difficult topics. Initially it introduces the reader to the fundamental concepts underlying performance and stability, including lift characteristics and estimation of drag, before moving on to a more detailed analysis of performance in both level and climbing flight. Pitching motion is then described followed by a detailed discussion of all aspects of both lateral and longitudinal stability and response. It finishes with an examination of inertial cross-coupling and automatic control and stabilization. The student is helped to think in three dimensions throughout the book by the use of illustrative examples. The progression from one degree of freedom to six degrees of freedom is gradually introduced. The result is an approach dealing specifically with all aspects of performance, stability and control that fills a gap in the current literature. It will be essential reading for all those embarking on degree level courses in aeronautical engineering and will be of interest to all with an interest in stability and dynamics, including those in commercial flying schools who require an insight into the performance of their aircraft. Ideal for undergraduate aeronautical engineers Three-dimensional thinking introduced through worked examples and simple situations | ||
500 | |a Includes bibliographical references (p. [285-286]) and index | ||
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650 | 7 | |a Stability of airplanes |2 fast | |
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Datensatz im Suchindex
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any_adam_object | |
author | Russell, J. B. |
author_facet | Russell, J. B. |
author_role | aut |
author_sort | Russell, J. B. |
author_variant | j b r jb jbr |
building | Verbundindex |
bvnumber | BV042315565 |
collection | ZDB-33-ESD ZDB-33-EBS |
ctrlnum | (OCoLC)162129605 (DE-599)BVBBV042315565 |
dewey-full | 629.132/36 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.132/36 |
dewey-search | 629.132/36 |
dewey-sort | 3629.132 236 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Verkehr / Transport |
format | Electronic eBook |
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institution | BVB |
isbn | 9780340631706 0340631708 0080538649 9780080538648 0470235985 |
language | English |
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spelling | Russell, J. B. Verfasser aut Performance and stability of aircraft J.B. Russell London Arnold 1996 1 Online-Ressource (xx, 294) txt rdacontent c rdamedia cr rdacarrier The performance, stability, control and response of aircraft are key areas of aeronautical engineering. This book provides a comprehensive overview to the underlying theory and application of what are often perceived to be difficult topics. Initially it introduces the reader to the fundamental concepts underlying performance and stability, including lift characteristics and estimation of drag, before moving on to a more detailed analysis of performance in both level and climbing flight. Pitching motion is then described followed by a detailed discussion of all aspects of both lateral and longitudinal stability and response. It finishes with an examination of inertial cross-coupling and automatic control and stabilization. The student is helped to think in three dimensions throughout the book by the use of illustrative examples. The progression from one degree of freedom to six degrees of freedom is gradually introduced. The result is an approach dealing specifically with all aspects of performance, stability and control that fills a gap in the current literature. It will be essential reading for all those embarking on degree level courses in aeronautical engineering and will be of interest to all with an interest in stability and dynamics, including those in commercial flying schools who require an insight into the performance of their aircraft. Ideal for undergraduate aeronautical engineers Three-dimensional thinking introduced through worked examples and simple situations Includes bibliographical references (p. [285-286]) and index Aeronautics / Mathematics fast Airplanes / Performance fast Stability of airplanes fast Mathematik Stability of airplanes Airplanes Performance Aeronautics Mathematics Flugzeug (DE-588)4017672-1 gnd rswk-swf Leistung (DE-588)4132608-8 gnd rswk-swf Stabilität (DE-588)4056693-6 gnd rswk-swf Flugzeug (DE-588)4017672-1 s Stabilität (DE-588)4056693-6 s 1\p DE-604 Leistung (DE-588)4132608-8 s 2\p DE-604 http://www.sciencedirect.com/science/book/9780340631706 Verlag 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 | Russell, J. B. Performance and stability of aircraft Aeronautics / Mathematics fast Airplanes / Performance fast Stability of airplanes fast Mathematik Stability of airplanes Airplanes Performance Aeronautics Mathematics Flugzeug (DE-588)4017672-1 gnd Leistung (DE-588)4132608-8 gnd Stabilität (DE-588)4056693-6 gnd |
subject_GND | (DE-588)4017672-1 (DE-588)4132608-8 (DE-588)4056693-6 |
title | Performance and stability of aircraft |
title_auth | Performance and stability of aircraft |
title_exact_search | Performance and stability of aircraft |
title_full | Performance and stability of aircraft J.B. Russell |
title_fullStr | Performance and stability of aircraft J.B. Russell |
title_full_unstemmed | Performance and stability of aircraft J.B. Russell |
title_short | Performance and stability of aircraft |
title_sort | performance and stability of aircraft |
topic | Aeronautics / Mathematics fast Airplanes / Performance fast Stability of airplanes fast Mathematik Stability of airplanes Airplanes Performance Aeronautics Mathematics Flugzeug (DE-588)4017672-1 gnd Leistung (DE-588)4132608-8 gnd Stabilität (DE-588)4056693-6 gnd |
topic_facet | Aeronautics / Mathematics Airplanes / Performance Stability of airplanes Mathematik Airplanes Performance Aeronautics Mathematics Flugzeug Leistung Stabilität |
url | http://www.sciencedirect.com/science/book/9780340631706 |
work_keys_str_mv | AT russelljb performanceandstabilityofaircraft |