Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method
Author: John W. Edwards
Publisher:
Published: 1996
Total Pages: 22
ISBN-13:
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Author: John W. Edwards
Publisher:
Published: 1996
Total Pages: 22
ISBN-13:
DOWNLOAD EBOOKAuthor: H. Sobieczky
Publisher: Springer Science & Business Media
Published: 2012-12-06
Total Pages: 406
ISBN-13: 9401000174
DOWNLOAD EBOOK"Symposium Transsonicum" was founded by Klaus Oswatitsch four decades ago when there was clearly a need for a systematic treatment of flow problems in the higher speed regime in aeronautics. The first conference in 1962 brought together scientists concerned with fundamental problems involving the sonic flow speed regime. Results of the conference provided an understanding of some basic tran sonic phenomena by proposing mathematical methods that allowed for the de velopment of practical calculations. The "Transonic Controversy" (about shock free flows) was still an open issue after this meeting. In 1975 the second symposium was held, by then there was much understanding in how to avoid shocks in a steady plane flow to be designed, but still very little was known in unsteady phenomena due to a lack of elucidating experiments. A third meeting in 1988 reflected the availability oflarger computers which allowed the numerical analysis of flows with shocks to a reasonable accuracy. Because we are trying to keep Oswatitsch's heritage in science alive especially in Gottingen, we were asked by the aerospace research community to organize another symposium. Much had been achieved already in the knowledge, techno logy and applications in transonics, so IUT AM had to be convinced that a fourth meeting would not just be a reunion of old friends reminiscing some scientific past. The scientific committee greatly supported my efforts to invite scientists ac tively working in transonic problems which still pose substantial difficulties to ae rospace and turbomachinery industry.
Author: Robert Clark
Publisher: Springer Science & Business Media
Published: 2004-09-30
Total Pages: 788
ISBN-13: 9781402020391
DOWNLOAD EBOOKIn this new edition, the fundamental material on classical linear aeroelasticity has been revised. Also new material has been added describing recent results on the research frontiers dealing with nonlinear aeroelasticity as well as major advances in the modelling of unsteady aerodynamic flows using the methods of computational fluid dynamics and reduced order modeling techniques. New chapters on aeroelasticity in turbomachinery and aeroelasticity and the latter chapters for a more advanced course, a graduate seminar or as a reference source for an entrée to the research literature.
Author: Lu Ting
Publisher: World Scientific
Published: 2005
Total Pages: 302
ISBN-13: 9812703438
DOWNLOAD EBOOKHonoring the contributions of one of the field''s leading experts, Lu Ting, this indispensable volume contains important new results at the cutting edge of research. A wide variety of significant new analytical and numerical results in critical areas are presented, including point vortex dynamics, superconductor vortices, cavity flows, vortex breakdown, shock/vortex interaction, wake flows, magneto-hydrodynamics, rotary wake flows, and hypersonic vortex phenomena. The book will be invaluable for those interested in the state of the art of vortex dominated flows, both from a theoretical and applied perspective. Professor Lu Ting and Joe Keller have worked together for over 40 years. In their first joint work entitled OC Periodic vibrations of systems governed by nonlinear partial differential equationsOCO, perturbation analysis and bifurcation theory were used to determine the frequencies and modes of vibration of various physical systems. The novelty was the application to partial differential equations of methods which, previously, had been used almost exclusively on ordinary differential equations. Professsor Lu Ting is an expert in both fluid dynamics and the use of matched asymptotic expansions. His physical insight into fluid flows has led the way to finding the appropriate mathematical simplications used in the solutions to many difficult flow problems."
Author:
Publisher:
Published: 1997
Total Pages: 180
ISBN-13:
DOWNLOAD EBOOKAuthor: Earl H. Dowell
Publisher: Springer Nature
Published: 2021-10-16
Total Pages: 828
ISBN-13: 3030742369
DOWNLOAD EBOOKThis book is the sixth edition. It is suitable for one or more courses at the advanced undergraduate level and graduate level to cover the field of aeroelasticity. It is also of value to the research scholar and engineering practitioner who wish to understand the state of the art in the field. This book covers the basics of aeroelasticity or the dynamics of fluid–structure interaction. While the field began in response to the rapid development of aviation, it has now expanded into many branches of engineering and scientific disciplines and treats physical phenomena from aerospace engineering, bioengineering, civil engineering, and mechanical engineering in addition to drawing the attention of mathematicians and physicists. The basic questions addressed are dynamic stability and response of fluid structural systems as revealed by both linear and nonlinear mathematical models and correlation with experiment. The use of scaled models and full-scale experiments and tests play a key role where theory is not considered sufficiently reliable.
Author:
Publisher:
Published: 1997
Total Pages: 232
ISBN-13:
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Publisher:
Published: 1997
Total Pages: 180
ISBN-13:
DOWNLOAD EBOOKAuthor: Eleanor C. Wynne
Publisher:
Published: 1993
Total Pages: 232
ISBN-13:
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Publisher:
Published: 2003
Total Pages: 610
ISBN-13:
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