This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft.
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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.
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Anbieter: World of Books (was SecondSale), Montgomery, IL, USA
Hardback. Zustand: Good. 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. Artikel-Nr. CIN052119590XG
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Anbieter: GreatBookPricesUK, Woodford Green, Vereinigtes Königreich
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Hardback. Zustand: New. 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. Artikel-Nr. LU-9780521195904
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Hardcover. Zustand: Brand New. 1st edition. 272 pages. 10.00x7.00x0.80 inches. In Stock. Artikel-Nr. x-052119590X
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Buch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - 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. Artikel-Nr. 9780521195904
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Anbieter: Kennys Bookstore, Olney, MD, USA
Zustand: New. 2011. 2nd Edition. Hardcover. Series: Cambridge Aerospace Series. 272 pages, 121 b/w illus. 19 tables 73 exercises. This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft. Cateogry: (U) Tertiary Education (US: College). BIC Classification: TGB; TRP. Dimension: 260 x 182 x 20. Weight: 732. . . . . . Books ship from the US and Ireland. Artikel-Nr. V9780521195904
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Anbieter: Rarewaves.com UK, London, Vereinigtes Königreich
Hardback. Zustand: New. 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. Artikel-Nr. LU-9780521195904
Anzahl: Mehr als 20 verfügbar
Anbieter: Kennys Bookshop and Art Galleries Ltd., Galway, GY, Irland
Zustand: New. 2011. 2nd Edition. Hardcover. Series: Cambridge Aerospace Series. 272 pages, 121 b/w illus. 19 tables 73 exercises. This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft. Cateogry: (U) Tertiary Education (US: College). BIC Classification: TGB; TRP. Dimension: 260 x 182 x 20. Weight: 732. . . . . . Artikel-Nr. V9780521195904
Anzahl: Mehr als 20 verfügbar