Analysis Of Low Speed Unsteady Airfoil Flows

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Analysis of Low-Speed Unsteady Airfoil Flows

Analysis of Low-Speed Unsteady Airfoil Flows
Author :
Publisher : Springer
Total Pages : 226
Release :
ISBN-10 : 3540803556
ISBN-13 : 9783540803553
Rating : 4/5 (553 Downloads)

Book Synopsis Analysis of Low-Speed Unsteady Airfoil Flows by : Tuncer Cebeci

Download or read book Analysis of Low-Speed Unsteady Airfoil Flows written by Tuncer Cebeci and published by Springer. This book was released on 2009-09-02 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt: The standard textbooks on aerodynamics usually omit any discussion of un steady aerodynamics or, at most, consider it only in a single chapter, based on two justifications. The first is that unsteady aerodynamics should be regarded as a specialized subject required "only" in connection with understanding and an alyzing aeroelastic phenomena such as flutter and gust response, and therefore should be dealt with in related specialist books. The second reason appears to be reluctance to discuss aerodynamics with the inclusion of the time-dependent terms in the conservation equations and the boundary conditions for fear that added complications may discourage the reader. We take the opposite view in this book and argue that a full understanding of the physics of lift generation is possible only by considering the unsteady aerody namics of the starting vortex generation process. Furthermore, certain "steady" flows are inherently unsteady in the presence of flow separation, as for example the unsteady flow caused by the Karman vortex shedding downstream of a cylin der and "static" airfoil stall which is an inherently unsteady flow phenomenon. Therefore, it stands to reason that a unified treatment of aerodynamics that yields steady-state aerodynamics as a special case offers advantages. This rea soning is strengthened by the developments in computational fluid dynamics over the past forty years, which showed that accurate steady-state solutions can be obtained efficiently by solving the unsteady flow equations.


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