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Beschreibung
This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. More than one hundred illustrations and tables help clarify the text and more than fifty problems enhance student learning. This text meets the need for an up-to-date treatment of structural dynamics and aeroelasticity for advanced undergraduate or beginning graduate aerospace engineering students.
This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. More than one hundred illustrations and tables help clarify the text and more than fifty problems enhance student learning. This text meets the need for an up-to-date treatment of structural dynamics and aeroelasticity for advanced undergraduate or beginning graduate aerospace engineering students.
Über den Autor
Dewey H. Hodges is a professor in the School of Aerospace Engineering at the Georgia Institute of Technology. He is the author of more than 170 refereed journal papers and three books, Nonlinear Composite Beam Theory (2006), Fundamentals of Structural Stability, with G. J. Simitses (2005) and Introduction to Structural Dynamics and Aeroelasticity, with G. Alvin Pierce (2002). His research spans the fields of aeroelasticity, dynamics, computational structural mechanics and structural dynamics, perturbation methods, computational optimal control and numerical analysis.
Inhaltsverzeichnis
1. Introduction; 2. Mechanics fundamentals; 3. Structural dynamics; 4. Static aeroelasticity; 5. Aeroelastic flutter.
Details
Erscheinungsjahr: 2013
Fachbereich: Fertigungstechnik
Genre: Importe, Technik
Rubrik: Naturwissenschaften & Technik
Medium: Taschenbuch
ISBN-13: 9781107617094
ISBN-10: 110761709X
Sprache: Englisch
Einband: Kartoniert / Broschiert
Autor: Hodges, Dewey H.
Pierce, G. Alvin
Hersteller: Cambridge University Press
Verantwortliche Person für die EU: Libri GmbH, Europaallee 1, D-36244 Bad Hersfeld, gpsr@libri.de
Maße: 254 x 178 x 15 mm
Von/Mit: Dewey H. Hodges (u. a.)
Erscheinungsdatum: 15.08.2013
Gewicht: 0,518 kg
Artikel-ID: 105511172

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