Computational Aeroelasticity: Modelling, Analysis and Design - Hardcover

Bureerat, Sujin

Hardcover

ISBN 10: 9819589029 ISBN 13: 9789819589029

Publisher: Springer, 2026

Synopsis

This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers.

About this title

About the Author

Sujin Bureerat received his Ph.D. in engineering from the University of Manchester, United Kingdom. His thesis is related to multidisciplinary optimization of a fin structure of a jet fighter taking account aeroelastic, buckling, and static structural design criteria. With more than 20 years as a researcher, he has published over 170 research papers indexed in Scopus while his research interests include multidisciplinary design optimization, reliability optimization, metaheuristics, surrogate modelling, aeroelasticity, aircraft design, and flight control and autopilot. He has performed over 700 reviews of more than 70 international journals. Sujin was awarded the TRF-OHEC-Clarivate Analytics Research Excellence Award in 2018 for his research in the field of engineering optimization. He was granted the TRF senior research scholar in 2019 and NRCT senior research scholar in 2022. His research topic for the senior research scholar is multidisciplinary design optimization for fixed-wing aircraft.

From the Back Cover

This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers.

Edition details

• Publisher: Springer
• Publication date: 2026
• Language: English
• ISBN 10: 9819589029
• ISBN 13: 9789819589029
• Binding: Hardcover
• Number of pages: 386