Introduction to Transonic Aerodynamics

Introduction to Transonic Aerodynamics
Author :
Publisher : Springer
Total Pages : 561
Release :
ISBN-10 : 9789401797474
ISBN-13 : 9401797471
Rating : 4/5 (74 Downloads)

Book Synopsis Introduction to Transonic Aerodynamics by : Roelof Vos

Download or read book Introduction to Transonic Aerodynamics written by Roelof Vos and published by Springer. This book was released on 2015-03-04 with total page 561 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics. Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter. The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.

High Angle of Attack Aerodynamics

High Angle of Attack Aerodynamics
Author :
Publisher : Springer Science & Business Media
Total Pages : 408
Release :
ISBN-10 : 9781461228240
ISBN-13 : 1461228247
Rating : 4/5 (40 Downloads)

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 Principles of Flight Vehicles

Aerodynamic Principles of Flight Vehicles
Author :
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Total Pages : 0
Release :
ISBN-10 : 1600869165
ISBN-13 : 9781600869167
Rating : 4/5 (65 Downloads)

Book Synopsis Aerodynamic Principles of Flight Vehicles by : A. G. Panaras

Download or read book Aerodynamic Principles of Flight Vehicles written by A. G. Panaras and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2012 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: In "Aerodynamic Principles of Flight Vehicles" Argyris Panaras examines the fundamentals of vortices and shock waves, aerodynamic estimation of lift and drag, airfoil theory, boundary layer control, and high-speed, high-temperature flow. Individual chapters address vortices in aerodynamics, transonic and supersonic flows, transonic/supersonic aircraft configurations, and high-supersonic/hypersonic flows, beginning with definitions and historical data, and then describing present-day status and current research challenges. Emphasis is given to flow control, to the evolution of flight vehicle shapes as flight speed has increased, and to discoveries that enabled breakthrough developments in flight. The book: examines why various equations and technologies were developed, explains major contributors in areas such as vortices and aircraft wakes, drag buildup, sonic boom, and shock wave-boundary layer interactions, among others, and helps readers apply concepts from the material to their own projects. Archival and encyclopedic, "Aerodynamic Principles of Flight Vehicles" is a superb reference for aeronautical students and professionals alike. Although most beneficial to readers with a working knowledge of aerodynamics, it is accessible to anyone with an introductory understanding of the field.

Fundamentals of Modern Unsteady Aerodynamics

Fundamentals of Modern Unsteady Aerodynamics
Author :
Publisher : Springer
Total Pages : 402
Release :
ISBN-10 : 9789811000188
ISBN-13 : 9811000182
Rating : 4/5 (88 Downloads)

Book Synopsis Fundamentals of Modern Unsteady Aerodynamics by : Ülgen Gülçat

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.

Introduction to Aircraft Flight Mechanics

Introduction to Aircraft Flight Mechanics
Author :
Publisher : AIAA
Total Pages : 666
Release :
ISBN-10 : 1600860788
ISBN-13 : 9781600860782
Rating : 4/5 (88 Downloads)

Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout

Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

Transonic Wind Tunnel Testing

Transonic Wind Tunnel Testing
Author :
Publisher :
Total Pages : 420
Release :
ISBN-10 : UVA:X030260513
ISBN-13 :
Rating : 4/5 (13 Downloads)

Book Synopsis Transonic Wind Tunnel Testing by : B. H. Goethert

Download or read book Transonic Wind Tunnel Testing written by B. H. Goethert and published by . This book was released on 2007 with total page 420 pages. Available in PDF, EPUB and Kindle. Book excerpt: Numerous aspects of transonic aerodynamics include wall interference corrections in conventional wind tunnels, subsonic flow in a variety of wind tunnels, and test results from transonic wind tunnels. 1961 edition.

An Introduction to Theoretical and Computational Aerodynamics

An Introduction to Theoretical and Computational Aerodynamics
Author :
Publisher : Courier Corporation
Total Pages : 484
Release :
ISBN-10 : 9780486317533
ISBN-13 : 0486317536
Rating : 4/5 (33 Downloads)

Book Synopsis An Introduction to Theoretical and Computational Aerodynamics by : Jack Moran

Download or read book An Introduction to Theoretical and Computational Aerodynamics written by Jack Moran and published by Courier Corporation. This book was released on 2013-04-22 with total page 484 pages. Available in PDF, EPUB and Kindle. Book excerpt: Concise text discusses properties of wings and airfoils in incompressible and primarily inviscid flow, viscid flows, panel methods, finite difference methods, and computation of transonic flows past thin airfoils. 1984 edition.