Aeroservoelasticity

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Geliefert zwischen Do., 09.04.2026 und Fr., 10.04.2026

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This monograph presents the state of the art in aeroservoelastic (ASE) modeling and analysis and develops a systematic theoretical and computational framework for use by researchers and practicing engineers. It is the first book to focus on the mathematical modeling of structural dynamics, unsteady aerodynamics, and control systems to evolve a generic procedure to be applied for ASE synthesis. Existing robust, nonlinear, and adaptive control methodology is applied and extended to some interesting ASE problems, such as transonic flutter and buffet, post-stall buffet and maneuvers, and flapping flexible wing.

The author derives a general aeroservoelastic plant via the finite-element structural dynamic model, unsteady aerodynamic models for various regimes in the frequency domain, and the associated state-space model by rational function approximations. For more advanced models, the full-potential, Euler, and Navier-Stokes methods for treating transonic and separated flows are also briefly addressed. Essential ASE controller design and analysis techniques are introduced to the reader, and an introduction to robust control-law design methods of LQG/LTR and H2/H synthesis is followed by a brief coverage of nonlinear control techniques of describing functions and Lyapunov functions. Practical and realistic aeroservoelastic application examples derived from actual experiments are included throughout.

Aeroservoelasiticity fills an important gap in the aerospace engineering literature and will be a valuable guide for graduate students and advanced researchers in aerospace engineering, as well as professional engineers, technicians, and test pilots in the aircraft industry and laboratories.


First book on aeroservoelastic modeling and analysis Presents aeroservoelasticity in the modern controls context by multivariable, state-space methods including robust, nonlinear, and adaptive control techniques Comprehensive and unique treatment of diverse unsteady aerodynamics and structural dynamics concepts, from first principles to numerical modeling Includes practical and realistic aeroservoelastic application examples derived from actual experiments Includes supplementary material: sn.pub/extras

Inhalt

Aeroservoelasticity.- Structural Modeling.- Unsteady Aerodynamic Modeling.- Finite-State Aeroelastic Modeling.- Linear Aeroelastic Control.- Nonlinear Aeroservoelastic Applications.- Appendices.- References.- Index.

Weitere Informationen

  • Allgemeine Informationen
    • GTIN 09781493944279
    • Genre Maths
    • Auflage Softcover reprint of the original 1st ed. 2015
    • Sprache Englisch
    • Lesemotiv Verstehen
    • Anzahl Seiten 318
    • Herausgeber Springer
    • Größe H237mm x B156mm x T19mm
    • Jahr 2016
    • EAN 9781493944279
    • Format Kartonierter Einband
    • ISBN 978-1-4939-4427-9
    • Titel Aeroservoelasticity
    • Autor Ashish Tewari
    • Untertitel Modeling and Control
    • Gewicht 530g

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