Introduction to Aeroelasticity

James DeLaurier (Autor)

Buch | Hardcover

184 Seiten

2024
CRC Press (Verlag)
978-1-032-70906-2 (ISBN)

Lieferbar (Termin unbekannt)
Versandkostenfrei
Auch auf Rechnung

Artikel merken

This book introduces the classical topics of aeroelasticity, beginning with elastic structural modeling and the way that wing and tail structures can diverge and deform due to aerodynamic, inertial, and control-surface deflections. It presents equation derivations in a step-by-step fashion, complemented by numerical and historical examples.

Introduction to Aeroelasticity introduces the classical topics of aeroelasticity, beginning with elastic structural modeling and the way that wing and tail structures can diverge and deform due to aerodynamic, inertial, and control-surface deflections.

Flutter is then described, first with an airfoil example with increasing complexity, and then for flutter predictions of finite wings with and without control surfaces.Single-degree-of-freedom flutter is also discussed, which includes cable “galloping,” Aeolian flutter, as well as plunging and pitching stall flutter. In all cases, the equation derivations proceed in a step-by-step fashion, complemented by several numerical (and historical) examples.

The book is intended to be a quantitative survey course for senior undergraduate and graduate students, as well as any engineer wishing a thorough introduction of the topic.

Instructors will be able to utilize a Solutions Manual and figure slides for their course based upin this book.

James DeLaurier has worked as an aerospace engineer, consultant, and professor. He received his PhD from Stanford University and has worked at McDonnell Aircraft, the NASA Ames Research Center, the Sheldahl Company, and Battelle Memorial Institute. Until his retirement in 2006, Dr. DeLaurier was a professor at the University of Toronto Institute for Aerospace Studies (UTIAS). His research topics have included aircraft design, lighter-than-air flight vehicles (airships and aerostats), flapping-wing aircraft, and remotely-piloted microwave-powered aircraft.

1. Introduction. 2. Structural Aspects: Stiffness and Flexibility. 3. Divergence. 4. Control Reversal. 5. Structural Dynamics. 6. Classical Flutter. 7. Single-Degree of Freedom Flutter. Appendix A. Lumped-Parameter Coupled Bending and Twisting. Appendix B. Flutter of the Representative Section with Control Surface.

Erscheinungsdatum	06.12.2024
Zusatzinfo	12 Tables, black and white; 132 Line drawings, black and white; 6 Halftones, black and white; 138 Illustrations, black and white
Verlagsort	London
Sprache	englisch
Maße	156 x 234 mm
Gewicht	520 g
Themenwelt	Mathematik / Informatik ► Mathematik ► Angewandte Mathematik
	Technik ► Bauwesen
	Technik ► Fahrzeugbau / Schiffbau
	Technik ► Luft- / Raumfahrttechnik
	Technik ► Maschinenbau
	Technik ► Umwelttechnik / Biotechnologie
ISBN-10	1-032-70906-5 / 1032709065
ISBN-13	978-1-032-70906-2 / 9781032709062
Zustand	Neuware