國立高雄大學圖資館 |

登入

回首頁

Fundamentals of aeroelasticity

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Fundamentals of aeroelasticityby Flávio D. Marques.
作者:	Marques, Flávio D.
出版者:	Cham :Springer Nature Switzerland :2025.
面頁冊數:	x, 183 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer Nature eBook
標題:	Aeroelasticity.
電子資源:	https://doi.org/10.1007/978-3-031-70951-7
ISBN:	9783031709517$q(electronic bk.)

Fundamentals of aeroelasticity
Marques, Flávio D.

Fundamentals of aeroelasticity[electronic resource] /by Flávio D. Marques. - Cham :Springer Nature Switzerland :2025. - x, 183 p. :ill. (some col.), digital ;24 cm. - Solid mechanics and its applications,v. 2792214-7764 ;. - Solid mechanics and its applications ;v. 152..

Static Stability of Airfoils and Wings -- Equilibrium of an elementary airfoil model -- Aeroelastic divergence -- Stability criteria of airfoil aeroelastic equilibrium -- Equilibrium of airfoil with control surface.

This book delves into the fundamentals of aeroelasticity, providing a modern foundation for education and research in aeronautical engineering. It begins with a brief introduction to aeroelasticity and then explores the static stability of airfoils and wings, using elementary models to solve fluid-structure interaction problems under equilibrium conditions. The dynamics of the typical aeroelastic section are examined, including modal analysis and dynamic characterization. Analytical and numerical aerodynamic models are discussed for unsteady aerodynamics, offering tools for studying stability phenomena and calculating aeroelastic responses. The text covers aeroelastic response and stability analysis, demonstrating coupled aerodynamic models' behavior under varying parameters and predicting flutter phenomena. The dynamic aeroelasticity of wings is analyzed, presenting a time-domain simulation model to show flutter conditions and aeroelastic modes. Appendices provide insights on finite element modeling of beams, self-excited systems, and surface interpolation methods, with numerous examples for result replication, though no specific computational tools are suggested.

ISBN: 9783031709517$q(electronic bk.)

Standard No.: 10.1007/978-3-031-70951-7doiSubjects--Topical Terms:

391338
Aeroelasticity.

LC Class. No.: TL574.A37

Dewey Class. No.: 629.132362

Fundamentals of aeroelasticity
LDR:02431nmm a2200337 a 4500 001 679106
003 DE-He213
005 20241225115226.0
006 m o d
007 cr nn 008maaau
008 251031s2025 sz s 0 eng d
020 $a 9783031709517$q(electronic bk.)
020 $a 9783031709500$q(paper)
024 7 $a 10.1007/978-3-031-70951-7 $2 doi
035 $a 978-3-031-70951-7
040 $a GP $c GP
041 0 $a eng
050 4 $a TL574.A37
072 7 $a TGMD $2 bicssc
072 7 $a SCI096000 $2 bisacsh
072 7 $a TGMD $2 thema
082 0 4 $a 629.132362 $2 23
090 $a TL574.A37 $b M357 2025
100 1 $a Marques, Flávio D. $3 992275
245 1 0 $a Fundamentals of aeroelasticity $h [electronic resource] / $c by Flávio D. Marques.
260 $a Cham : $b Springer Nature Switzerland : $b Imprint: Springer, $c 2025.
300 $a x, 183 p. : $b ill. (some col.), digital ; $c 24 cm.
490 1 $a Solid mechanics and its applications, $x 2214-7764 ; $v v. 279
505 0 $a Static Stability of Airfoils and Wings -- Equilibrium of an elementary airfoil model -- Aeroelastic divergence -- Stability criteria of airfoil aeroelastic equilibrium -- Equilibrium of airfoil with control surface.
520 $a This book delves into the fundamentals of aeroelasticity, providing a modern foundation for education and research in aeronautical engineering. It begins with a brief introduction to aeroelasticity and then explores the static stability of airfoils and wings, using elementary models to solve fluid-structure interaction problems under equilibrium conditions. The dynamics of the typical aeroelastic section are examined, including modal analysis and dynamic characterization. Analytical and numerical aerodynamic models are discussed for unsteady aerodynamics, offering tools for studying stability phenomena and calculating aeroelastic responses. The text covers aeroelastic response and stability analysis, demonstrating coupled aerodynamic models' behavior under varying parameters and predicting flutter phenomena. The dynamic aeroelasticity of wings is analyzed, presenting a time-domain simulation model to show flutter conditions and aeroelastic modes. Appendices provide insights on finite element modeling of beams, self-excited systems, and surface interpolation methods, with numerous examples for result replication, though no specific computational tools are suggested.
650 0 $a Aeroelasticity. $3 391338
650 1 4 $a Solid Mechanics. $3 825700
650 2 4 $a Engineering Mechanics. $3 913404
650 2 4 $a Mechanical Engineering. $3 273894
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer Nature eBook
830 0 $a Solid mechanics and its applications ; $v v. 152. $3 513892
856 4 0 $u https://doi.org/10.1007/978-3-031-70951-7
950 $a Engineering (SpringerNature-11647)