Fundamentals of Aeroelasticity (eBook)

Artikelnummer: 978-3-031-70951-7
Einband: PDF
Verfügbarkeit: Download, sofort verfügbar (Link per E-Mail)
CHF 94.50
decrease increase

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.

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.

Schreiben Sie Ihre eigene Bewertung
  • Nur registrierte Benutzer können Produkte bewerten
*
*
Schlecht
Sehr gut
*
*
*
*
VerlagSpringer International Publishing
EinbandPDF
Erscheinungsjahr2024
Seitenangabe183 S.
AusgabekennzeichenEnglisch
AbbildungenX, 183 p. 106 illus., 2 illus. in color.
Masse17'175 KB
PlattformPDF
ReiheSolid Mechanics and its Applications; Engineering; Engineering
AutorMarques, Flávio D.

Alle Bände der Reihe "Solid Mechanics and its Applications; Engineering; Engineering (R0)"

Über den Autor Flávio D. Marques

Dr. Flávio D. Marques graduated in Mechanical Engineering from the São Carlos Engineering School of the University of São Paulo, Brazil (1987), with a Master's degree in Mechanical Engineering from the University of São Paulo, Brazil (1993). He has a Ph.D. in Aerospace Engineering from the University of Glasgow, Scotland, UK (1997) and also worked as a structural analysis engineer in the EMBRAER (1988-1990). He has been an Associate Professor of the Department of Mechanical Engineering of the Engineering School of São Carlos of the University of São Paulo, Brazil, since 1999, teaching dynamics, aeroelasticity, and flight mechanics. His research interests focus on linear and nonlinear aeroelasticity, unsteady aerodynamics, aeronautical smart structures, and non-conventional control systems, with applications of neural networks, fuzzy logic, and genetic algorithms in aerospace problems.

Weitere Titel von Flávio D. Marques

Produktbewertungen
Nur registrierte Benutzer können Produkte bewerten