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Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce
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
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
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
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
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
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
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
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
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
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
Opac: Controlla la disponibilità qui