Elementary flight dynamics with an introduction to bifurcation and continuation methods:
"Preface Flight mechanics lies at the heart of aeronautics. It is the point of confluence of other disciplines within aerospace engineering and the gateway to aircraft design. Almost every curriculum in aerospace engineering includes two courses in flight mechanics...one on applied aerodynamics...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Boca Raton, FL
CRC Press
2022
|
| Ausgabe: | second edition |
| Schlagworte: | |
| Online-Zugang: | FHI01 Volltext |
| Zusammenfassung: | "Preface Flight mechanics lies at the heart of aeronautics. It is the point of confluence of other disciplines within aerospace engineering and the gateway to aircraft design. Almost every curriculum in aerospace engineering includes two courses in flight mechanics...one on applied aerodynamics and airplane performance and the other on airplane stability/control and flight dynamics. Having taught both these subjects for over two decades, the authors' experience can be summed up briefly in the following student response: 'These are the best subjects in the curriculum. When you teach it in class, everything is obvious, but when we go back and read the textbook, things get very confusing'. As we got down to decoding this statement, several questions emerged: - Why put students through the gruesome derivation of the sixdegree- of-freedom equations early in the course, preceded by the axis transformations, and followed by the small perturbation math, when the bulk of the course is focussed on the dynamic modes about straight and level flight trim, which can be easily presented without going this route? - Would it not be nicer to write the equations for the second-order modes in a manner similar to a spring-mass-damper system? Then, one could read off the stiffness and damping directly, which would also give the conditions for stability. - The definitions of 'static' and 'dynamic' stability have been the cause of much student heartbreak. With the second-order form of the equations, the requirement of positive stiffness is the same as the socalled 'static' stability condition, so why not drop the separate notion of static stability entirely? -".. |
| Beschreibung: | 1 Online-Ressource (xiii, 375 Seiten) Ill., graph. Darst. |
| ISBN: | 9781439886021 9781003096801 |
| DOI: | 10.1201/9781003096801 |
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| 245 | 1 | 0 | |a Elementary flight dynamics with an introduction to bifurcation and continuation methods |c Nandan K. Sinha, N. Ananthkrishnan |
| 250 | |a second edition | ||
| 264 | 1 | |a Boca Raton, FL |b CRC Press |c 2022 | |
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| 520 | |a "Preface Flight mechanics lies at the heart of aeronautics. It is the point of confluence of other disciplines within aerospace engineering and the gateway to aircraft design. Almost every curriculum in aerospace engineering includes two courses in flight mechanics...one on applied aerodynamics and airplane performance and the other on airplane stability/control and flight dynamics. Having taught both these subjects for over two decades, the authors' experience can be summed up briefly in the following student response: 'These are the best subjects in the curriculum. When you teach it in class, everything is obvious, but when we go back and read the textbook, things get very confusing'. As we got down to decoding this statement, several questions emerged: - Why put students through the gruesome derivation of the sixdegree- of-freedom equations early in the course, preceded by the axis transformations, and followed by the small perturbation math, when the bulk of the course is focussed on the dynamic modes about straight and level flight trim, which can be easily presented without going this route? - Would it not be nicer to write the equations for the second-order modes in a manner similar to a spring-mass-damper system? Then, one could read off the stiffness and damping directly, which would also give the conditions for stability. - The definitions of 'static' and 'dynamic' stability have been the cause of much student heartbreak. With the second-order form of the equations, the requirement of positive stiffness is the same as the socalled 'static' stability condition, so why not drop the separate notion of static stability entirely? -".. | ||
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Datensatz im Suchindex
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| author | Sinha, Nandan K. Ananthkrishnan, N. |
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| dewey-full | 629.132/3 |
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| id | DE-604.BV048550482 |
| illustrated | Illustrated |
| index_date | 2024-07-03T20:57:09Z |
| indexdate | 2024-07-10T09:41:13Z |
| institution | BVB |
| isbn | 9781439886021 9781003096801 |
| language | English |
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| physical | 1 Online-Ressource (xiii, 375 Seiten) Ill., graph. Darst. |
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| spelling | Sinha, Nandan K. Verfasser (DE-588)1137949376 aut Elementary flight dynamics with an introduction to bifurcation and continuation methods Nandan K. Sinha, N. Ananthkrishnan second edition Boca Raton, FL CRC Press 2022 1 Online-Ressource (xiii, 375 Seiten) Ill., graph. Darst. txt rdacontent c rdamedia cr rdacarrier "Preface Flight mechanics lies at the heart of aeronautics. It is the point of confluence of other disciplines within aerospace engineering and the gateway to aircraft design. Almost every curriculum in aerospace engineering includes two courses in flight mechanics...one on applied aerodynamics and airplane performance and the other on airplane stability/control and flight dynamics. Having taught both these subjects for over two decades, the authors' experience can be summed up briefly in the following student response: 'These are the best subjects in the curriculum. When you teach it in class, everything is obvious, but when we go back and read the textbook, things get very confusing'. As we got down to decoding this statement, several questions emerged: - Why put students through the gruesome derivation of the sixdegree- of-freedom equations early in the course, preceded by the axis transformations, and followed by the small perturbation math, when the bulk of the course is focussed on the dynamic modes about straight and level flight trim, which can be easily presented without going this route? - Would it not be nicer to write the equations for the second-order modes in a manner similar to a spring-mass-damper system? Then, one could read off the stiffness and damping directly, which would also give the conditions for stability. - The definitions of 'static' and 'dynamic' stability have been the cause of much student heartbreak. With the second-order form of the equations, the requirement of positive stiffness is the same as the socalled 'static' stability condition, so why not drop the separate notion of static stability entirely? -".. SCIENCE / Mechanics / General bisacsh TECHNOLOGY & ENGINEERING / Electrical bisacsh TECHNOLOGY & ENGINEERING / Mechanical bisacsh Aerodynamics Bifurcation theory Continuation methods SCIENCE / Mechanics / General TECHNOLOGY & ENGINEERING / Electrical TECHNOLOGY & ENGINEERING / Mechanical Stabilität (DE-588)4056693-6 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Flugmechanik (DE-588)4154760-3 gnd rswk-swf Flugmechanik (DE-588)4154760-3 s DE-604 Flugzeug (DE-588)4017672-1 s Stabilität (DE-588)4056693-6 s Ananthkrishnan, N. Verfasser aut Erscheint auch als Druck-Ausgabe 978-0-367-56207-6 https://doi.org/10.1201/9781003096801 Verlag URL des Erstveröffentlichers Volltext |
| spellingShingle | Sinha, Nandan K. Ananthkrishnan, N. Elementary flight dynamics with an introduction to bifurcation and continuation methods SCIENCE / Mechanics / General bisacsh TECHNOLOGY & ENGINEERING / Electrical bisacsh TECHNOLOGY & ENGINEERING / Mechanical bisacsh Aerodynamics Bifurcation theory Continuation methods SCIENCE / Mechanics / General TECHNOLOGY & ENGINEERING / Electrical TECHNOLOGY & ENGINEERING / Mechanical Stabilität (DE-588)4056693-6 gnd Flugzeug (DE-588)4017672-1 gnd Flugmechanik (DE-588)4154760-3 gnd |
| subject_GND | (DE-588)4056693-6 (DE-588)4017672-1 (DE-588)4154760-3 |
| title | Elementary flight dynamics with an introduction to bifurcation and continuation methods |
| title_auth | Elementary flight dynamics with an introduction to bifurcation and continuation methods |
| title_exact_search | Elementary flight dynamics with an introduction to bifurcation and continuation methods |
| title_exact_search_txtP | Elementary flight dynamics with an introduction to bifurcation and continuation methods |
| title_full | Elementary flight dynamics with an introduction to bifurcation and continuation methods Nandan K. Sinha, N. Ananthkrishnan |
| title_fullStr | Elementary flight dynamics with an introduction to bifurcation and continuation methods Nandan K. Sinha, N. Ananthkrishnan |
| title_full_unstemmed | Elementary flight dynamics with an introduction to bifurcation and continuation methods Nandan K. Sinha, N. Ananthkrishnan |
| title_short | Elementary flight dynamics with an introduction to bifurcation and continuation methods |
| title_sort | elementary flight dynamics with an introduction to bifurcation and continuation methods |
| topic | SCIENCE / Mechanics / General bisacsh TECHNOLOGY & ENGINEERING / Electrical bisacsh TECHNOLOGY & ENGINEERING / Mechanical bisacsh Aerodynamics Bifurcation theory Continuation methods SCIENCE / Mechanics / General TECHNOLOGY & ENGINEERING / Electrical TECHNOLOGY & ENGINEERING / Mechanical Stabilität (DE-588)4056693-6 gnd Flugzeug (DE-588)4017672-1 gnd Flugmechanik (DE-588)4154760-3 gnd |
| topic_facet | SCIENCE / Mechanics / General TECHNOLOGY & ENGINEERING / Electrical TECHNOLOGY & ENGINEERING / Mechanical Aerodynamics Bifurcation theory Continuation methods Stabilität Flugzeug Flugmechanik |
| url | https://doi.org/10.1201/9781003096801 |
| work_keys_str_mv | AT sinhanandank elementaryflightdynamicswithanintroductiontobifurcationandcontinuationmethods AT ananthkrishnann elementaryflightdynamicswithanintroductiontobifurcationandcontinuationmethods |