04506nam a22005415i 4500 978-3-031-53379-2 DE-He213 20251030112044.0 cr nn 008mamaa 240516s2024 sz | s |||| 0|eng d 9783031533792 978-3-031-53379-2 10.1007/978-3-031-53379-2 doi TA349-359 TGB bicssc TEC009070 bisacsh TGB thema Gennaretti, Massimo. author. aut http://id.loc.gov/vocabulary/relators/aut 76895 Fundamentals of Aeroelasticity [electronic resource] / by Massimo Gennaretti. 1st ed. 2024. Cham : Springer Nature Switzerland : Imprint: Springer, 2024. XIII, 298 p. 71 illus. online resource. text txt rdacontent computer c rdamedia online resource cr rdacarrier text file PDF rda Part 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. This 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. Mechanics, Applied. Aerospace engineering. 66335 Astronautics. 66336 Dynamics. 65524 Nonlinear theories. 65525 Engineering Mechanics. Aerospace Technology and Astronautics. 66339 Applied Dynamical Systems. 65530 SpringerLink (Online service) Springer Nature eBook Printed edition: 9783031533785 Printed edition: 9783031533808 Printed edition: 9783031534409 https://doi.org/10.1007/978-3-031-53379-2 ZDB-2-ENG ZDB-2-SXE 59893 59893