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Record Nr. |
UNINA9910458027903321 |
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Autore |
Hodges Dewey H. |
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Titolo |
Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce [[electronic resource]] |
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Pubbl/distr/stampa |
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Cambridge : , : Cambridge University Press, , 2011 |
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ISBN |
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1-107-21462-9 |
1-139-11939-7 |
1-283-29847-3 |
9786613298478 |
1-139-12296-7 |
0-511-99711-6 |
1-139-11722-X |
1-139-12788-8 |
1-139-11069-1 |
1-139-11286-4 |
1-139-11505-7 |
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Edizione |
[Second edition.] |
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Descrizione fisica |
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1 online resource (xxi, 247 pages) : digital, PDF file(s) |
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Collana |
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Cambridge aerospace series ; ; 15 |
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Disciplina |
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Soggetti |
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Space vehicles - Dynamics |
Aeroelasticity |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from publisher's bibliographic system (viewed on 05 Oct 2015). |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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Cover; Title; Copyright; Contents; Figures; Tables; Foreword; From First Edition; Addendum for Second Edition; 1 Introduction; 2 Mechanics Fundamentals; 2.1 Particles and Rigid Bodies; 2.1.1 Newton's Laws; 2.1.2 Euler's Laws and Rigid Bodies; 2.1.3 Kinetic Energy; 2.1.4 Work; 2.1.5 Lagrange's Equations; 2.2 Modeling the Dynamics of Strings; 2.2.1 Equations of Motion; 2.2.2 Strain Energy; 2.2.3 Kinetic Energy; 2.2.4 Virtual Work of Applied, Distributed Force; 2.3 Elementary Beam Theory; 2.3.1 Torsion; 2.3.2 Bending; 2.4 Composite Beams |
2.4.1 Constitutive Law and Strain Energy for Coupled Bending and Torsion2.4.2 Inertia Forces and Kinetic Energy for Coupled Bending and Torsion; 2.4.3 Equations of Motion for Coupled Bending and Torsion; |
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2.5 The Notion of Stability; 2.6 Systems with One Degree of Freedom; 2.6.1 Unforced Motion; 2.6.2 Harmonically Forced Motion; 2.7 Epilogue; Problems; 3 Structural Dynamics; 3.1 Uniform String Dynamics; 3.1.1 Standing Wave (Modal) Solution; 3.1.2 Orthogonality of Mode Shapes; 3.1.3 Using Orthogonality; 3.1.4 Traveling Wave Solution; 3.1.5 Generalized Equations of Motion |
3.1.6 Generalized Force3.1.7 Example Calculations of Forced Response; 3.2 Uniform Beam Torsional Dynamics; 3.2.1 Equations of Motion; 3.2.2 Boundary Conditions; 3.2.3 Example Solutions for Mode Shapes and Frequencies; 3.2.4 Calculation of Forced Response; 3.3 Uniform Beam Bending Dynamics; 3.3.1 Equation of Motion; 3.3.2 General Solutions; 3.3.3 Boundary Conditions; 3.3.4 Example Solutions for Mode Shapes and Frequencies; 3.3.5 Calculation of Forced Response; 3.4 Free Vibration of Beams in Coupled Bending and Torsion; 3.4.1 Equations of Motion; 3.4.2 Boundary Conditions |
3.5 Approximate Solution Techniques3.5.1 The Ritz Method; 3.5.2 Galerkin's Method; 3.5.3 The Finite Element Method; 3.6 Epilogue; Problems; 4 Static Aeroelasticity; 4.1 Wind-Tunnel Models; 4.1.1 Wall-Mounted Model; 4.1.2 Sting-Mounted Model; 4.1.3 Strut-Mounted Model; 4.1.4 Wall-Mounted Model for Application to Aileron Reversal; 4.2 Uniform Lifting Surface; 4.2.1 Steady-Flow Strip Theory; 4.2.2 Equilibrium Equation; 4.2.3 Torsional Divergence; 4.2.4 Airload Distribution; 4.2.5 Aileron Reversal; 4.2.6 Sweep Effects; 4.2.7 Composite Wings and Aeroelastic Tailoring; 4.3 Epilogue; Problems |
5 Aeroelastic Flutter5.1 Stability Characteristics from Eigenvalue Analysis; 5.2 Aeroelastic Analysis of a Typical Section; 5.3 Classical Flutter Analysis; 5.3.1 One-Degree-of-Freedom Flutter; 5.3.2 Two-Degree-of-Freedom Flutter; 5.4 Engineering Solutions for Flutter; 5.4.1 The k Method; 5.4.2 The p-k Method; 5.5 Unsteady Aerodynamics; 5.5.1 Theodorsen's Unsteady Thin-Airfoil Theory; 5.5.2 Finite-State Unsteady Thin-Airfoil Theory of Peters et al.; 5.6 Flutter Prediction via Assumed Modes; 5.7 Flutter Boundary Characteristics; 5.8 Structural Dynamics, Aeroelasticity, and Certification |
5.8.1 Ground-Vibration Tests |
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Sommario/riassunto |
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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. |
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2. |
Record Nr. |
UNINA9910792289203321 |
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Titolo |
Japanese animation : East Asian perspectives / / edited by Masao Yokota and Tze-yue G. Hu |
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Pubbl/distr/stampa |
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Jackson, Mississippi : , : University Press of Mississippi, , 2013 |
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ISBN |
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Descrizione fisica |
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1 online resource (326 p.) |
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Classificazione |
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Disciplina |
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Soggetti |
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Animated films - Japan - History and criticism |
Animated television programs - Japan - History and criticism |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Description based upon print version of record. |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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Animation Studies and Animation History in Japan -- Pioneers of Japanese Animation -- Popular Culture, East-West Expressions, and Tezuka Osamu -- Female Characters and Transnational Identities -- Artistic Animation and Expression in Japan -- Japan's First Commercial Animation Studio after the Second World War: Toei. |
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Sommario/riassunto |
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"Japanese Animation: East Asian Perspectives makes available for the first time to English readership a selection of viewpoints from media practitioners, designers, educators, and scholars working in the East Asian Pacific. This collection not only engages a multidisciplinary approach in understanding the subject of Japanese animation but also shows ways to research, teach, and more fully explore this multidimensional world. Presented in six sections, the translated essays cross-reference each other. The collection adopts a wide range of critical, historical, practical, and experimental approaches. This variety provides a creative and fascinating edge for both specialist and nonspecialist readers. Contributors' works share a common relevance, interest, and involvement despite their regional considerations and the different modes of analysis demonstrated. They form a composite of teaching and research ideas on Japanese animation"-- |
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