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020 _a9783031533792
_9978-3-031-53379-2
024 7 _a10.1007/978-3-031-53379-2
_2doi
050 4 _aTA349-359
072 7 _aTGB
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aTGB
_2thema
100 1 _aGennaretti, Massimo.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_976895
245 1 0 _aFundamentals of Aeroelasticity
_h[electronic resource] /
_cby Massimo Gennaretti.
250 _a1st ed. 2024.
264 1 _aCham :
_bSpringer Nature Switzerland :
_bImprint: Springer,
_c2024.
300 _aXIII, 298 p. 71 illus.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
505 0 _aPart I: Aeroelastic modelling and solution methods -- CHAPTER 1 Introduction to Aeroelasticity -- CHAPTER 2 The Wing Typical Section -- CHAPTER 3 Finite Wings -- CHAPTER 4 The Panel Method for Wing Aeroelasticity -- CHAPTER 5 Elements of Aeroservoelasticity -- CHAPTER 6 Finite Wings in Compressible Flows -- CHAPTER 7 An Introduction to Rotary-Wing Aeroelasticity -- Part II: Mathematical tools and methods -- CHAPTER 8 Elements of the Calculus of Variations -- CHAPTER 9 Elements of Differential Geometry -- CHAPTER 10 Notes on Galërkin's Method.
520 _aThis textbook provides the fundamentals of aeroelasticity, with particular attention to problems of interest to aeronautical engineering. The mathematical methods and tools applicable to the modern modeling of general aeroelastic problems are presented, discussed, and applied to fixed-wing aircraft configurations. It is composed of ten chapters divided into two parts: (I) aeroelastic modeling and analysis and (ii) mathematical tools. The six chapters that compose the first part start from the historical background of the discipline, then present the methods for coupling structural dynamics and unsteady aerodynamics for the aeroelastic modeling of the typical wing section, and then extend them to applications for twisted, tapered, swept finite-wing configurations. In this context, particular attention is paid to the presentation, interpretation, and discussion of the available unsteady sectional aerodynamic theories, both in the time and frequency domain, providing a broad scenario of the formulations that can be used for conventional and non-conventional aerodynamic/aeroelastic applications. For a modern view of aeroelasticity, a significant portion of the textbook deals with illustration and discussion of three-dimensional aerodynamic theories and computational methods for the determination of unsteady aerodynamic loads over lifting bodies in incompressible and compressible flows, as well as to the introduction and explanation of methodologies for the identification of reduced-order, state-space aerodynamic/aeroelastic operators suitable for stability (flutter) analysis and control purposes. A chapter is dedicated to the theories and approaches for aeroservoelastic modeling. In the second part of the textbook, additional chapters provide theoretical insights on topics that enrich the multidisciplinary knowledge related to widely applied methods and models for the analysis and solution of aeroelastic problems. The book serves as a reference tool for master's degree students in aeronautical/aerospace engineering, as well as researchers in the field of aeroelasticity.
650 0 _aMechanics, Applied.
650 0 _aAerospace engineering.
_966335
650 0 _aAstronautics.
_966336
650 0 _aDynamics.
_965524
650 0 _aNonlinear theories.
_965525
650 1 4 _aEngineering Mechanics.
650 2 4 _aAerospace Technology and Astronautics.
_966339
650 2 4 _aApplied Dynamical Systems.
_965530
710 2 _aSpringerLink (Online service)
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783031533785
776 0 8 _iPrinted edition:
_z9783031533808
776 0 8 _iPrinted edition:
_z9783031534409
856 4 0 _uhttps://doi.org/10.1007/978-3-031-53379-2
912 _aZDB-2-ENG
912 _aZDB-2-SXE
999 _c59893
_d59893