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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 : 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 : 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 : 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 : Sidney M. Harmon
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)
Download or read book Theoretical Relations Between the Stability Derivatives of a Wing in Direct and in Reverse Supersonic Flow written by Sidney M. Harmon and published by . This book was released on 1949 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investivation is made for thin flate-plate wings for steady vertical and longitudinal motions, setady rolling and pitching, and motions in which the wing is accelerating uniformly in the vertical direction.
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.
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 : Aleksandr Ivanovich Nekrasov
Publisher :
ISBN 13 :
Total Pages : 592 pages
Book Rating : 4.F/5 ( download)
Download or read book Theory of Wings in Nonstationary Flow written by Aleksandr Ivanovich Nekrasov and published by . This book was released on 1947 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper gives an overview of equations for vibration and flutter affecting airplane wings in nonstationary flow.
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 : 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 : Maxwell Alfred Heaslet
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms written by Maxwell Alfred Heaslet and published by . This book was released on 1948 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Author : J. J. Chattot
Publisher : Springer
ISBN 13 : 9401798257
Total Pages : 625 pages
Book Rating : 4.4/5 (17 download)
Download or read book Theoretical and Applied Aerodynamics written by J. J. Chattot and published by Springer. This book was released on 2015-03-31 with total page 625 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: -The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. - The linearized theories for compressible subsonic and supersonic aerodynamics. - The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. - Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations. There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows. A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.
Author : John B. McDevitt
Publisher :
ISBN 13 :
Total Pages : 67 pages
Book Rating : 4.:/5 (249 download)
Download or read book The Linearized Subsonic Flow about Symmetrical Nonlifting Wing-body Combinations written by John B. McDevitt and published by . This book was released on 1957 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt: Methods are presented for determining the linearized subsonic flow about symmetrical, nonlifting wing-body combinations. The wing is represented by a suitable planar distribution of elementary sources in accordance with the usual assumptions of linearized, thin-airfoil theory. The required boundary condition for tangential flow at the body surface is met by distributing along the body axis suitable distributions of three-dimensional sources and multipoles. As part of the present analysis, a theory is presented for determining the flow about circular or noncircular bodies by the use of axially distributed sources and multipoles. The flow over thin, nonlifting airfoils having symmetrical profiles is also studied in considerable detail, and it is shown that the concept of the oblique source filament can be used in obtaining numerical results for wings having tapered as well as untapered plan forms. A comparison of theory and experiment is made for two 45 degree sweptback wings in combination with basic Sears-Haack bodies of revolution and in combination with the basic bodies indented according to Whitcomb's transonic area rule. The effect of indenting the body on the pressure distribution near the wing-body juncture is of particular interest for sweptwing and body combinations. The effect of the area-rule indentation was to adjust the pressure field near the body so that the wing surface isobars tended to follow the local sweep lines of the wing.
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.
