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Fundamentals of aeroelasticity

Record Type:	Electronic resources : Monograph/item
Title/Author:	Fundamentals of aeroelasticity/ by Massimo Gennaretti.
Author:	Gennaretti, Massimo.
Published:	Cham :Springer Nature Switzerland : : 2024.,
Description:	xiii, 298 p. :ill., digital ;24 cm.
[NT 15003449]:	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.
Contained By:	Springer Nature eBook
Subject:	Aeroelasticity. -
Online resource:	https://doi.org/10.1007/978-3-031-53379-2
ISBN:	9783031533792

Fundamentals of aeroelasticity
Gennaretti, Massimo.

Fundamentals of aeroelasticity[electronic resource] /by Massimo Gennaretti. - Cham :Springer Nature Switzerland :2024. - xiii, 298 p. :ill., digital ;24 cm.

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.

ISBN: 9783031533792

Standard No.: 10.1007/978-3-031-53379-2doiSubjects--Topical Terms:

834363
Aeroelasticity.

LC Class. No.: TL574.A37

Dewey Class. No.: 629.132362

Fundamentals of aeroelasticity
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100 1 $a Gennaretti, Massimo. $3 3717592
245 1 0 $a Fundamentals of aeroelasticity $h [electronic resource] / $c by Massimo Gennaretti.
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300 $a xiii, 298 p. : $b ill., digital ; $c 24 cm.
505 0 $a 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.
520 $a 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.
650 0 $a Aeroelasticity. $3 834363
650 1 4 $a Engineering Mechanics. $3 3538834
650 2 4 $a Aerospace Technology and Astronautics. $3 928116
650 2 4 $a Applied Dynamical Systems. $3 3538870
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773 0 $t Springer Nature eBook
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