Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce |
Autore | Hodges Dewey H. |
Edizione | [Second edition.] |
Pubbl/distr/stampa | Cambridge : , : Cambridge University Press, , 2011 |
Descrizione fisica | 1 online resource (xxi, 247 pages) : digital, PDF file(s) |
Disciplina | 629.134/31 |
Collana | Cambridge aerospace series |
Soggetto topico |
Aeroelasticitat
Vehicles espacials - Dinàmica Space vehicles - Dynamics Aeroelasticity |
ISBN |
1-139-92979-8
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 |
Classificazione | TEC009000 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
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; 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 |
Altri titoli varianti | Introduction to structural dynamics & aeroelasticity |
Record Nr. | UNINA-9910829075303321 |
Hodges Dewey H. | ||
Cambridge : , : Cambridge University Press, , 2011 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Material and thickness grading for aeroelastic tailoring of the common research model wing box / / Bret K. Stanford, Christine V. Jutte |
Autore | Stanford Bret K. |
Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014 |
Descrizione fisica | 1 online resource (14 pages) : color illustrations |
Collana | NASA/TM |
Soggetto topico |
Functionally gradient materials
Aeroelasticity Wing planforms Aircraft design Modulus of elasticity Yield strength |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910702734403321 |
Stanford Bret K. | ||
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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A modern course in aeroelasticity / / edited by Earl H. Dowell |
Edizione | [6th ed.] |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2021] |
Descrizione fisica | 1 online resource (828 pages) |
Disciplina | 629.132362 |
Collana | Solid Mechanics and Its Applications |
Soggetto topico |
Aeroelasticity
Mathematical modelling |
ISBN | 3-030-74236-9 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910523773903321 |
Cham, Switzerland : , : Springer, , [2021] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel : theory and experiment / / Benjamin D. Goldman, Robert C. Scott, Earl H. Dowell |
Autore | Goldman Benjamin D. |
Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 |
Descrizione fisica | 1 online resource (44 pages) : color illustrations |
Collana | NASA/TM |
Soggetto topico |
Thermal protection
Aerodynamic brakes Aeroelasticity Heat shielding Inflatable structures High temperature tests Flutter |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Altri titoli varianti | Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel |
Record Nr. | UNINA-9910702659303321 |
Goldman Benjamin D. | ||
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Nonstationary dynamics data analysis with wavelet-SVD filtering / / Marty Brenner, Dale Groutage |
Autore | Brenner Marty <1955-> |
Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , April 2001 |
Descrizione fisica | 1 online resource (16 pages) : illustrations |
Collana | NASA TM |
Soggetto topico |
Aeroelasticity
Aeroservoelasticity Wavelet analysis Probability distribution functions Density distribution |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Altri titoli varianti | Nonstationary dynamics data analysis with wavelet- singular value decomposition filtering |
Record Nr. | UNINA-9910692978703321 |
Brenner Marty <1955-> | ||
Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , April 2001 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Novel control effectors for truss braced wing / / Edward V. White, Rakesh K. Kapania, Shiv Joshi |
Autore | White Edward V. |
Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 |
Descrizione fisica | 1 online resource (xxiii, 212 pages) : color illustrations |
Collana | NASA/CR |
Soggetto topico |
Lateral control
Flight conditions Swept wings Aeroelasticity Ailerons |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910704019403321 |
White Edward V. | ||
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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A numerical model of unsteady, subsonic aeroelastic behavior [[electronic resource] /] / by Thomas W. Strganac |
Autore | Strganac Thomas W |
Edizione | [[Aug. 1987 ed.]] |
Pubbl/distr/stampa | [Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1987] |
Descrizione fisica | 1 online resource (xii, 110 pages) : illustrations (some color) |
Collana | NASA TM |
Soggetto topico |
Aerodynamic loads
Aeroelasticity Equations of motion Lattices (mathematics) Mathematical models Prediction analysis techniques Vortices Wings |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910700819803321 |
Strganac Thomas W | ||
[Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1987] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Quiet High Speed Fan II (QHSF II) : final report / / Karen Kontos, Don Weir, and Dave Ross |
Autore | Kontos Karen |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
Descrizione fisica | 1 online resource (xiv, 183 pages) : illustrations (some color) |
Collana | NASA/CR |
Soggetto topico |
Low speed wind tunnels
Acoustic properties Aeroacoustics Aeroelasticity Guide vanes Turbofans Structural design Tip speed |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Altri titoli varianti | Quiet High Speed Fan II |
Record Nr. | UNINA-9910702342303321 |
Kontos Karen | ||
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Re-computation of numerical results contained in NACA report no. 496 / / Boyd Perry, III |
Autore | Perry Boyd |
Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2015 |
Descrizione fisica | 1 online resource (112 pages) : color illustrations |
Collana | NASA/TP |
Soggetto topico |
Aeroelasticity
Aeronautical engineering Theodorsen transformation Complex variables Flutter analysis |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Altri titoli varianti | Re-computation of numerical results contained in National Advisory Committee for Aeronautics report no. 496 |
Record Nr. | UNINA-9910703962003321 |
Perry Boyd | ||
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2015 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Rotary wing structural dynamics and aeroelasticity [[electronic resource] /] / Richard L. Bielawa |
Autore | Bielawa Richard L |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2006 |
Descrizione fisica | xix, 749 p. : ill |
Disciplina | 629.132/362 |
Collana | AIAA education series |
Soggetto topico |
Helicopters - Aerodynamics
Aeroelasticity |
Soggetto genere / forma | Electronic books. |
ISBN |
1-62870-117-X
1-60086-237-3 1-60086-109-1 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910456605503321 |
Bielawa Richard L | ||
Reston, Va., : American Institute of Aeronautics and Astronautics, c2006 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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