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Author : Sergeǐ Mikhaǐlovich Belotserkovskiǐ
Publisher : Springer
ISBN 13 : 1489962999
Total Pages : 236 pages
Book Rating : 4.4/5 (899 download)
Download or read book The Theory of Thin Wings in Subsonic Flow written by Sergeǐ Mikhaǐlovich Belotserkovskiǐ and published by Springer. This book was released on 2013-12-11 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sergei M. Belotserkovskii
Publisher :
ISBN 13 : 9780306302916
Total Pages : 250 pages
Book Rating : 4.3/5 (29 download)
Download or read book Theory of Thin Wings in Subsonic Flow written by Sergei M. Belotserkovskii and published by . This book was released on 1995-12-31 with total page 250 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sergeĭ Mikhaĭlovich Belot︠s︡erkovskiĭ
Publisher :
ISBN 13 :
Total Pages : 230 pages
Book Rating : 4.:/5 (112 download)
Download or read book The Theory of Thin Wings in Subsonic Flow written by Sergeĭ Mikhaĭlovich Belot︠s︡erkovskiĭ and published by . This book was released on 1967 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sergeĭ Mikhaĭlovich Belot︠s︡erkovskiĭ
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (122 download)
Download or read book The Theory of Thin Wings in Subsonic Flows written by Sergeĭ Mikhaĭlovich Belot︠s︡erkovskiĭ and published by . This book was released on with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Elie Carafoli
Publisher : Elsevier
ISBN 13 : 1483160270
Total Pages : 611 pages
Book Rating : 4.4/5 (831 download)
Download or read book Wing Theory in Supersonic Flow written by Elie Carafoli and published by Elsevier. This book was released on 2013-10-22 with total page 611 pages. Available in PDF, EPUB and Kindle. Book excerpt: Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the characteristics of drag, lift, and moments for various shapes of the trailing edge line. This book discusses as well the wings of ordinary shapes, delta wings, yawed wings, polygonal wings, trapezoid wings, and arrow-head or swept-back wings. The final chapter deals with a delta wing with a central fusiform body. This book is a valuable resource for teachers, students, and specialists engaged in modern aerodynamics.
Author : Robert Thomas Jones
Publisher : Princeton University Press
ISBN 13 : 1400860776
Total Pages : 227 pages
Book Rating : 4.4/5 (8 download)
Download or read book Wing Theory written by Robert Thomas Jones and published by Princeton University Press. This book was released on 2014-07-14 with total page 227 pages. Available in PDF, EPUB and Kindle. Book excerpt: Originator of many of the theories used in modern wing design, Robert T. Jones surveys the aerodynamics of wings from the early theories of lift to modern theoretical developments. This work covers the behavior of wings at both low and high speeds, including the range from very low Reynolds numbers to the determination of minimum drag at supersonic speed. Emphasizing analytical techniques, Wing Theory provides invaluable physical principles and insights for advanced students, professors, and aeronautical engineers, as well as for scientists involved in computational approaches to the subject. This book is based on over forty years of theoretical and practical work performed by the author and other leading researchers in the field of aerodynamics. Originally published in 1990. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : Holt Ashley
Publisher : Courier Corporation
ISBN 13 : 0486648990
Total Pages : 306 pages
Book Rating : 4.4/5 (866 download)
Download or read book Aerodynamics of Wings and Bodies written by Holt Ashley and published by Courier Corporation. This book was released on 1965-01-01 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt: This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.
Author : Y C Fung
Publisher : Courier Dover Publications
ISBN 13 : 0486469360
Total Pages : 516 pages
Book Rating : 4.4/5 (864 download)
Download or read book An Introduction to the Theory of Aeroelasticity written by Y C Fung and published by Courier Dover Publications. This book was released on 2008-10-17 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt: Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Author : Milton D. Van Dyke
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (672 download)
Download or read book Subsonic Edges in Thin-wing and Slender-body Theory written by Milton D. Van Dyke and published by . This book was released on 1954 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: A simple technique is presented for correcting the results of thin-wing theory near round or sharp edges at which the normal component of free-stream velocity is subsonic. The flow in planes normal to such edges is actually brought to rest, but thin-wing theory instead predicts infinite velocities. Furthermore, corresponding to the circulatory flow around leading edges, thin-wing theory predicts additional singularities that do not actually exist for round edges and exceed their true strength for sharp edges. All these singularities grow worse if one formally attempts to improve the solution by iteration. To correct these defects, the formal thin-wing solution is here rendered uniformly valid by comparing with exact solutions for simple profiles having the same nose shape. In this way Lighthill's rule for correcting the surface speed on round-nosed airfoils in incompressible flow is extended to higher approximations, to compressible flow, to three-dimensional wings, and to sharp edges. Corresponding results for slender bodies of revolution are considered briefly; in particular, the rules for round-nosed airfoils in incompressble flow are shown to apply also to round-nosed bodies of revolution.
Author : Ye P. Aksenov
Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (227 download)
Download or read book Theory of Thin Wing in a Supersonic Flow with Consideration of the Non-Equilibrium State of Excitation of Oscillating Degrees of Freedom written by Ye P. Aksenov and published by . This book was released on 1978 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ülgen Gülçat
Publisher : Springer
ISBN 13 : 9811000182
Total Pages : 402 pages
Book Rating : 4.8/5 (11 download)
Download or read book Fundamentals of Modern Unsteady Aerodynamics written by Ülgen Gülçat and published by Springer. This book was released on 2015-10-31 with total page 402 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this book, the author introduces the concept of unsteady aerodynamics and its underlying principles. He provides the readers with a comprehensive review of the fundamental physics of free and forced unsteadiness, the terminology and basic equations of aerodynamics ranging from incompressible flow to hypersonics. The book also covers modern topics related to the developments made in recent years, especially in relation to wing flapping for propulsion. The book is written for graduate and senior year undergraduate students in aerodynamics and also serves as a reference for experienced researchers. Each chapter includes ample examples, questions, problems and relevant references. The treatment of these modern topics has been completely revised end expanded for the new edition. It now includes new numerical examples, a section on the ground effect, and state-space representation.
Author : Lazãr Dragos
Publisher : Springer Science & Business Media
ISBN 13 : 9781402016639
Total Pages : 626 pages
Book Rating : 4.0/5 (166 download)
Download or read book Mathematical Methods in Aerodynamics written by Lazãr Dragos and published by Springer Science & Business Media. This book was released on 2003 with total page 626 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book provides a solid and unitary mathematical foundation of the basic and advanced principles of aerodynamics. The densities of the fundamental solutions are determined from singular integral equations. The fundamental solutions method in aerodynamics was considered for the first time and used by the author in over 30 papers published in prestigious journals (e.g. QAM, AIAA, ZAMM, etc) in order to develop a unitary theory. The boundary element method is used for numerical approximations in compressible aerodynamics. The text incorporates several original contributions, among other traditional mathematical methods. The book also represents a comprehensive presentation of research results since the seminal books on aerodynamics of Ashley and Landahl (1965) and Katz & Plotkin (1991). A rigorous mathematical approach is used to present and explain classic and modern results in this field of science. The author has therefore conceived several appendices on the Distribution Theory, the singular Integral Equations Theory, the Finite Part, Gauss Quadrature Formulae, etc. The book is concluded by a relevant bibliographical list which is especially useful for researchers. The book is aimed primarily at applied mathematicians, aeronautical engineers and space science researchers. The text may be used also as a comprehensive introduction to the mathematical foundations fo aerodynamics, by graduate students n engineering and fluid dynamics with a strong mathematical background.
Author : Doris Cohen
Publisher : Princeton University Press
ISBN 13 : 1400874947
Total Pages : 251 pages
Book Rating : 4.4/5 (8 download)
Download or read book High Speed Wing Theory written by Doris Cohen and published by Princeton University Press. This book was released on 2015-12-08 with total page 251 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 988 pages
Book Rating : 4.E/5 ( download)
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 988 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ira H. Abbott
Publisher : Courier Corporation
ISBN 13 : 0486134997
Total Pages : 704 pages
Book Rating : 4.4/5 (861 download)
Download or read book Theory of Wing Sections written by Ira H. Abbott and published by Courier Corporation. This book was released on 2012-04-26 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt: Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
Author : Raymond L. Bisplinghoff
Publisher : Courier Corporation
ISBN 13 : 0486783162
Total Pages : 544 pages
Book Rating : 4.4/5 (867 download)
Download or read book Principles of Aeroelasticity written by Raymond L. Bisplinghoff and published by Courier Corporation. This book was released on 2013-10-17 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
Author : Frank S. Malvestuto
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.3/5 (91 download)
Download or read book Theoretical Lift and Damping in Roll of Thin Sweptback Wings of Arbitrary Taper and Sweep at Supersonic Speeds written by Frank S. Malvestuto and published by . This book was released on 1949 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design curves are presented which permit rapid estimation of the lift-curve slope and damping-in-roll derivative for given values of aspect ratio, taper ratio, Mach number, and leading edge sweep.
