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Aerodynamics of Wings and Bodies

Aerodynamics of Wings and Bodies
Author: Holt Ashley
Publisher: Courier Corporation
Total Pages: 306
Release: 1965-01-01
Genre: Technology & Engineering
ISBN: 0486648990

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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.


Introductory Aerodynamics and Hydrodynamics of Wings and Bodies

Introductory Aerodynamics and Hydrodynamics of Wings and Bodies
Author: Frederick O. Smetana
Publisher: AIAA
Total Pages: 270
Release: 1997
Genre: Aerodynamics
ISBN: 9781600860836

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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.


High Angle of Attack Aerodynamics

High Angle of Attack Aerodynamics
Author: Josef Rom
Publisher: Springer Science & Business Media
Total Pages: 408
Release: 2012-12-06
Genre: Science
ISBN: 1461228247

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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.


Theoretical Aerodynamics

Theoretical Aerodynamics
Author: L. M. Milne-Thomson
Publisher: Courier Corporation
Total Pages: 482
Release: 2012-04-30
Genre: Technology & Engineering
ISBN: 0486151832

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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.


Applied Hydro- and Aeromechanics

Applied Hydro- and Aeromechanics
Author: Oskar Karl Gustav Tietjens
Publisher: Courier Corporation
Total Pages: 338
Release: 1957-01-01
Genre: Technology & Engineering
ISBN: 048660375X

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Prandtl was one of the great theorists of aerodynamics and this work has long been considered one of the finest introductory works in the field. Topics include flow through pipes, Prandtl's own work on boundary layers, drag, airfoil theory, and entry conditions for flow in a pipe.


Wing Theory in Supersonic Flow

Wing Theory in Supersonic Flow
Author: Elie Carafoli
Publisher: Elsevier
Total Pages: 611
Release: 2013-10-22
Genre: Technology & Engineering
ISBN: 1483160270

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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.


An Introduction to Flapping Wing Aerodynamics

An Introduction to Flapping Wing Aerodynamics
Author: Wei Shyy
Publisher: Cambridge University Press
Total Pages: 321
Release: 2013-08-19
Genre: Technology & Engineering
ISBN: 1107067987

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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).