Aerodynamics of Wings and Bodies

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Publisher : Courier Corporation
ISBN 13 : 0486648990
Total Pages : 306 pages
Book Rating : 4.4/5 (866 download)

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Book Synopsis Aerodynamics of Wings and Bodies by : Holt Ashley

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.

Aerodynamics of Wings and Bodies

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Author :
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (299 download)

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Book Synopsis Aerodynamics of Wings and Bodies by : Holt Ashley

Download or read book Aerodynamics of Wings and Bodies written by Holt Ashley and published by . This book was released on 1965 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Introductory Aerodynamics and Hydrodynamics of Wings and Bodies

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Author :
Publisher : AIAA
ISBN 13 : 9781600860836
Total Pages : 270 pages
Book Rating : 4.8/5 (68 download)

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Book Synopsis Introductory Aerodynamics and Hydrodynamics of Wings and Bodies by : Frederick O. Smetana

Download or read book Introductory Aerodynamics and Hydrodynamics of Wings and Bodies written by Frederick O. Smetana and published by AIAA. This book was released on 1997 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation This textbook and its six supporting computer programs provide theoretical modeling of the aerodynamic characteristics of wings and bodies at low Mach numbers. The approach presented directly helps engineering students improve problem-solving skills by teaching them to discern the necessary steps associated with solving analytical problems. The book also presents a justification and rationale for validating end results that leave the student with an understanding of the answer. The text differs from others by providing interactive computer programs that allow the student to conduct trade studies. It provides case-specific software that permits the student to do considerably more characteristic analysis of user-selected wings and bodies than is possible with other introductory textbooks. In addition, the algorithms are capable of working problems at a level well beyond those typically solved by hand in other textbooks. This approach allows students to determine easily the effects of modifying parameters and geometry. Another benefit of using this textbook is the understanding students gain of the capabilities of large industrial codes.

Theoretical Aerodynamics

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Publisher : Courier Corporation
ISBN 13 : 0486151832
Total Pages : 464 pages
Book Rating : 4.4/5 (861 download)

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Book Synopsis Theoretical Aerodynamics by : L. M. Milne-Thomson

Download or read book Theoretical Aerodynamics written by L. M. Milne-Thomson and published by Courier Corporation. This book was released on 2012-04-30 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt: An excellent introduction to inviscid airflow using potential theory, this book is a classic in its field. Complete reprint of the revised 1966 edition, which brings the subject up to date.

High Angle of Attack Aerodynamics

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Author :
Publisher : Springer Science & Business Media
ISBN 13 : 1461228247
Total Pages : 408 pages
Book Rating : 4.4/5 (612 download)

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Book Synopsis High Angle of Attack Aerodynamics by : Josef Rom

Download or read book High Angle of Attack Aerodynamics written by Josef Rom and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 408 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.

Aerodynamic-center Considerations of Wings and Wing-body Combinations

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Author :
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic-center Considerations of Wings and Wing-body Combinations by : John E. Lamar

Download or read book Aerodynamic-center Considerations of Wings and Wing-body Combinations written by John E. Lamar and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wing Theory in Supersonic Flow

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Publisher : Elsevier
ISBN 13 : 1483160270
Total Pages : 608 pages
Book Rating : 4.4/5 (831 download)

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Book Synopsis Wing Theory in Supersonic Flow by : Elie Carafoli

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 608 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.

Aerodynamics of the Airplane

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Author :
Publisher : Courier Dover Publications
ISBN 13 : 0486823709
Total Pages : 209 pages
Book Rating : 4.4/5 (868 download)

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Book Synopsis Aerodynamics of the Airplane by : Clark B. Millikan

Download or read book Aerodynamics of the Airplane written by Clark B. Millikan and published by Courier Dover Publications. This book was released on 2018-05-16 with total page 209 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written on the eve of World War II, this brief but intensive introduction by one of the founders of the Jet Propulsion Laboratory deals with the basic problems of aerodynamics. 1941 edition.

An Introduction to Flapping Wing Aerodynamics

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Publisher : Cambridge University Press
ISBN 13 : 1107067987
Total Pages : pages
Book Rating : 4.1/5 (7 download)

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Book Synopsis An Introduction to Flapping Wing Aerodynamics by : Wei Shyy

Download or read book An Introduction to Flapping Wing Aerodynamics written by Wei Shyy and published by Cambridge University Press. This book was released on 2013-08-19 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: This is an ideal book for graduate students and researchers interested in the aerodynamics, structural dynamics and flight dynamics of small birds, bats and insects, as well as of micro air vehicles (MAVs), which present some of the richest problems intersecting science and engineering. The agility and spectacular flight performance of natural flyers, thanks to their flexible, deformable wing structures, as well as to outstanding wing, tail and body coordination, is particularly significant. To design and build MAVs with performance comparable to natural flyers, it is essential that natural flyers' combined flexible structural dynamics and aerodynamics are adequately understood. The primary focus of this book is to address the recent developments in flapping wing aerodynamics. This book extends the work presented in Aerodynamics of Low Reynolds Number Flyers (Shyy et al. 2008).

Classical Aerodynamic Theory

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Publisher :
ISBN 13 :
Total Pages : 324 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Classical Aerodynamic Theory by :

Download or read book Classical Aerodynamic Theory written by and published by . This book was released on 1979 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamics for engineering students

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Author :
Publisher :
ISBN 13 :
Total Pages : 458 pages
Book Rating : 4.:/5 (916 download)

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Book Synopsis Aerodynamics for engineering students by : Edward Lewis Houghton

Download or read book Aerodynamics for engineering students written by Edward Lewis Houghton and published by . This book was released on 1978 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA TN D-3581

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Author :
Publisher :
ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (861 download)

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Book Synopsis NASA TN D-3581 by : John E. Lamar

Download or read book NASA TN D-3581 written by John E. Lamar and published by . This book was released on 1968 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Engineering Analysis of Flight Vehicles

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Publisher : Courier Corporation
ISBN 13 : 0486166538
Total Pages : 402 pages
Book Rating : 4.4/5 (861 download)

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Book Synopsis Engineering Analysis of Flight Vehicles by : Holt Ashley

Download or read book Engineering Analysis of Flight Vehicles written by Holt Ashley and published by Courier Corporation. This book was released on 2013-05-27 with total page 402 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Written by one of the leading aerospace educators of our time, each sentence is packed with information. An outstanding book." — Private Pilot "Illuminated throughout by new twists in explaining familiar concepts, helpful examples and intriguing ‘by-the-ways.’ A fine book." — Canadian Aeronautics and Space Journal This classic by a Stanford University educator and a pioneer of aerospace engineering introduces the complex process of designing atmospheric flight vehicles. An exploration of virtually every important subject in the fields of subsonic, transonic, supersonic, and hypersonic aerodynamics and dynamics, the text demonstrates how these topics interface and how they complement one another in atmospheric flight vehicle design. The mathematically rigorous treatment is geared toward graduate-level students, and it also serves as an excellent reference. Problems at the end of each chapter encourage further investigation of the text’s material, the study of fresh ideas, and the exploration of new areas.

Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 646 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds by : John R. Spreiter

Download or read book Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds written by John R. Spreiter and published by . This book was released on 1949 with total page 646 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.

Wing Theory

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Publisher : Princeton University Press
ISBN 13 : 1400860776
Total Pages : 227 pages
Book Rating : 4.4/5 (8 download)

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Book Synopsis Wing Theory by : Robert Thomas Jones

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.

Aerodynamic Components of Aircraft at High Speeds

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Publisher : Princeton University Press
ISBN 13 : 1400879906
Total Pages : 863 pages
Book Rating : 4.4/5 (8 download)

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Book Synopsis Aerodynamic Components of Aircraft at High Speeds by : Allen F. Donovan

Download or read book Aerodynamic Components of Aircraft at High Speeds written by Allen F. Donovan and published by Princeton University Press. This book was released on 2015-12-08 with total page 863 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. 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.

Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0

Download Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 PDF Online Free

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Publisher :
ISBN 13 :
Total Pages : 164 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 by : Leland H. Jorgensen

Download or read book Experimental Aerodynamic Characteristics for Slender Bodies with Thin Wings at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 written by Leland H. Jorgensen and published by . This book was released on 1976 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: