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 upon this book.
Sprache
Verlagsort
Verlagsgruppe
Zielgruppe
Für höhere Schule und Studium
Postgraduate and Undergraduate Advanced
Illustrationen
6 s/w Photographien bzw. Rasterbilder, 132 s/w Zeichnungen, 12 s/w Tabellen, 138 s/w Abbildungen
12 Tables, black and white; 132 Line drawings, black and white; 6 Halftones, black and white; 138 Illustrations, black and white
Maße
Höhe: 240 mm
Breite: 161 mm
Dicke: 15 mm
Gewicht
ISBN-13
978-1-032-70906-2 (9781032709062)
Copyright in bibliographic data and cover images is held by Nielsen Book Services Limited or by the publishers or by their respective licensors: all rights reserved.
Schweitzer Klassifikation
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.
