Louis Melveille Milne-Thomson, Theoretical Aerodynamics
430 pages | Publisher: Dover Publications | 4th ed., rev. and enl edition (June 1973) Language: English | ISBN: 048661980X | pdf | 25,7 mb
Classic in field covers airfoils, subsonic and supersonic flow round a wing, aircraft as a whole, etc.
Nearly 400 exercises & Illustrations!
A classic in its field, Professor Milne-Thomson`s university text and reference book has long been one of the basic works.
This is the completer reprinting of the revised (1966) edition which brings the subject up to date, including a complete and probably unique chapter on conical flow round sweptback wings.
* Offers a readable, thorough overview of basic aerodynamics, with numerous discussions of aviation history and development
* Includes new coverage of the Computational Fluid Dynamics (CFD) and illustrations to help explain the material
* More than a dozen "design boxes" draw the reader's attention and illustrate the practical applications
Elements of Aerodynamics of Supersonic Flows (Dover Phoenix Editions)
By Antonio Ferri
* Publisher: Dover Publications
* Number Of Pages: 448
* Publication Date: 2005-08-26
* ISBN-10 / ASIN: 0486442802
* ISBN-13 / EAN: 9780486442808
Product Description:
Written by an expert on gas dynamics and compressibility, this study of the theory and physical phenomena of supersonic flows is presented from the practical engineering point of view. It explains the theory of both two- and three-dimensional flow and applications to a variety of aeronautical engineering problems. 1949 edition
Soon after its foundation in 1952, the Advisory Group for Aeronautical Research
and Development recognized the need for a comprehensive publication on tlight test
techniques and the associated instrumentation. Under the direction of the AGARD
Flight Test Panel (now the Flight Mechanics Panel), a Flight Test Manual was published
in the years 1954 to 1956. The Manual was divided into four volumes: I. Performance,
11. Stability and Control, III. Instrumentation C&dog, and IV. Instrumentation Systems.
Since then flight test instrumentation has developed rapidly in a broad field of
sophisticated techniques. In view of this development the flight Test Instrumentation
Committee of the Flight Mechanics Panel wa8 asked in 1968 to update Volumes III and
IV of the Flight Test Manual. Upon the advice of the Committee, the Panel decided that
Volume III would not be continued and that Volume IV would be replaced by a series
of separately published monographs on selected subjects of flight test instrumentation:
the AGARD Flight Test Instrumentation Series. The first volume of this Series gives a
general introduction to the basic principles of flight test instrumentation engineering and
is composed from contributions by several specialized authors. Each of the other volumes
provides a more detailed treatise by a specialist on a selected instrumentation subject.
Mr W.D.hlace and Mr A.Pool were willing to accept the responsibility of editing the
Series, and Prof. D.Bosman assisted them in editing the introductory volume. AGARD
was fortunate in fmding competent editors and authors willing to contribute their
knowledge and to spend considerable time lo the preparation of this Series.
It is hoped that this Series will satisfy the existing need for special&d documentation
in the field of fIight test instrumentation and as such may promote a better understanding
between the flight test engineer and the instrumentation and data processing
specialists. Such understanding is essential for the efficient design and execution of flight
test programs.
The efforts of the Flight Test Instrumentation Committee members and the assistance
of the Flight Mechanics Panel in the preparation of this Series are greatly
appreciated.
T. VAN OOSTEROM
Member of the Flight Mechanics Panel
Chairman of the Flight Test
Instrumentation Committee
ill
* Publisher: North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
* Number Of Pages: 160
* Publication Date: 1973
* ISBN-10 / ASIN: B0007AEVJ4
* Publisher: Ungar Pub Co
* Number Of Pages: 351
* Publication Date: 1981-06
* ISBN-10 / ASIN: 0804442754
* ISBN-13 / EAN: 9780804442756 Book Description:
Clearly written and well illustrated, this book provides the reader with a physical understanding of helicopter behavior, and a capability to quantitatively predict such behavior Written primarily for engineers and researchers, the book has also found wide readership amongst people, such as pilots and middle-level managers in industry and government, whose work requires them to have more than a general, qualitative understanding of the whys and wherefores of helicopter flight. Much of its success is credited to its approach which carefully guides the reader midway between a verbal, non-quantitative treatment on one hand, and a complex and highly mathematical exposition on the other. The emphasis on fundamentals makes the book an ideal, indeed necessary, first step towards the study or use of more sophisticated and comprehensive treatments
By H. W. Liepmann, A. Roshko
* Publisher: John Wiley & Sons Inc
* Number Of Pages: 456
* Publication Date: 1957
* ISBN-10 / ASIN: 0471534609
* ISBN-13 / EAN: 9780471534600 Book Description:
First-rate text covers introductory concepts from thermodynamics, one-dimensional gas dynamics and one-dimensional wave motion, waves in supersonic flow, flow in ducts and wind tunnels, methods of measurement, the equations of frictionless flow, small-perturbation theory, transonic flow, and much more. For advanced undergraduate or graduate physics and engineering students with at least a working knowledge of calculus and basic physics. Exercises demonstrate application of material in text.
Asymptotic Theory of Supersonic Viscous Gas Flows (Aerospace Engineering)
By Vladimir Neyland
* Publisher: Butterworth-Heinemann
* Number Of Pages: 560
* Publication Date: 2008-01-08
* ISBN-10 / ASIN: 0750685131
* ISBN-13 / EAN: 9780750685139 Book Description:
This is the first book in English devoted to the latest developments in fluid mechanics and aerodynamics. Written by the leading authors in the field, based at the renowned Central Aerohydrodynamic Institute in Moscow, it deals with viscous gas flow problems that arise from supersonic flows. These complex problems are central to the work of researchers and engineers dealing with new aircraft and turbomachinery development (jet engines, compressors and other turbine equipment). The book presents the latest asymptotical models, simplified Navier-Stokes equations and viscous-inviscid interaction theroies and will be of critical interest to researchers, engineers, academics and advanced graduate students in the areas of fluid mechanics, compressible flows, aerodynamics and aircraft design, applied mathematics and computational fluid dynamics.
Key features
* The first book in English to cover the latest methodology for incopressible flow analysis of high speed aerodynamics, an essential topic for those working on new generation aircraft and turbomachinery
* Authors are internationally recognised as the leading figures in the field
* Includes a chapter introducing asymptotical methods to enable advanced level students to use the book
Written by best-selling author, John D. Anderson, Jr., this book covers the subject of sustained hypersonic flight, the technology behind the Space Shuttle and other high speed flight vehicles. Anderson's book offers timely and up-to-date information on hypersonic flow-an area that has grown explosively in the last decade.
Hypersonic Aerothermodynamics - Aiaa Education Series
Hypersonic Aerothermodynamics - Aiaa Education Series
Hypersonic Aerothermodynamics
(Aiaa Education Series)
By John J. Bertin
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 608
* Publication Date: 1993-09
* ISBN-10 / ASIN: 1563470365
* ISBN-13 / EAN: 9781563470363
Book Description:
The first four chapters present general information characterizing hypersonic flows, discuss numerical formulations of varying degrees of rigor in computational fluid dynamics (CFD) codes, and discuss the strengths and limitations of the various types of hypersonic experimentation. Other chapters cover the stagnation-region flowfield, the inviscid flowfield, the boundary layer, the aerodynamic forces and moments, viscous/inviscid interactions and shock/shock interactions, and a review of aerothermodynamics phenomena and their role in the design of a hypersonic vehicle. Sample exercises and homework problems are presented throughout the text
Advanced Dynamics
(Aiaa Education Series)
By Shuh-Jing Ying
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 366
* Publication Date: 1997
* ISBN-10 / ASIN: 1563472244
* ISBN-13 / EAN: 9781563472244
Book Description: Advanced Dynamics is recognized as an important subject of study for all engineering students and professionals in competitive university programs and throughout the industry. This textbook adeptly explains the fundamental laws of motion, but goes a step beyond by covering new topics such as gyroscopic effects, missile trajectories, interplanetary missions, multistage rockets, and use of numerical methods. In addition, theories such as the rotation operator are taken to a new degree and developed further, far surpassing comparable textbooks.
The book balances theory and application and relates all subjects to practical problems, real-world situations, and recent advances that affect everyday life. This text distinguishes itself with a more complete introduction to recent developments in dynamics, new and practical applications to help the reader remember key theories and uses, and an appreciation that the subject matter is riddled with ongoing problems that need new solutions. These distinguishing features make Advanced Dynamics more complete, interesting, and understandable than existing textbooks and resource materials. Problems appear at the end of each chapter, and a complimentary solutions manual is available for professors.
Advanced Dynamics is also written for those engineers who want to update their knowledge and stay current of the changes in the field, but do not have the opportunity to attend formal classes. The reader will take away a thorough understanding of the foundation of mechanical engineering, which is necessary to read and assimilate scholarly papers and leading articles published in journals and peer-reviewed magazines
.
رئوس مطالب:
* Review of Fundamental Principles * Kinematics and Dynamics of a Particle
* Dynamics of a System of Particles
* Lagrange’s Equations and the Variational Principle
* Rockets and Space Vehicles
* Matrices, Tensors, Dyadics, and Rotation Operators
* Dynamics of a Rigid Body
* Fundamentals of Small Oscillations
* Vibration of Systems with Multiple Degrees-of-Freedom
* Special Relativity Theory
* Appendix A: Runge–Kutta Method
* Appendix B: Stoke’s Theorem
* Appendix C: Planetary Data
* Appendix D: Determinants and Matrices
* Appendix E: Method of Partial Fractions
* Appendix F: Tables of Fourier and Laplace Transforms
* Appendix G: Contour Integration and Inverse Laplace Transform
* Appendix H: Bessel Functions
* Appendix I: Instructions for Computer Programs
* Appendix J: Further Reading
* Index
The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. Missile Aerodynamics, a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more.
J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc
Basic Helicopter Aerodynamics: An Account of First Principles in the Fluid Mechanics and Flight Dynamics of the Single Rotor Helicopter
By J. Seddon, Simon Newman,
* Publisher: Blackwell Science
* Number Of Pages: 160
* Publication Date: 2001-06
* ISBN / ASIN: 063205283X
$142.88
Book Description:
This volume is an excellent introduction to the aerodynamics of helicopters. Basic Helicopter Aerodynamics provides an account of the first principles in the fluid mechanics and flight dynamics of single-rotor helicopters. The text is intended to provide, in a short volume, an introduction to the theory of rotary-wing aircraft for use by undergraduate and graduate students, while providing a detailed description of the physical phenomena involved. The text assumes that the reader already has some knowledge of differences between the fixed- and rotary-wing aircraft. Many diagrams, drawings, graphs, and representative sets of data augment the text
Aerodynamics of Wings and Bodies (Dover Books on Engineering)
By Holt Ashley, Marten Landahl
Publisher: Dover Publications
Number Of Pages: 288
Publication Date: 1985-07-01
ISBN-10 / ASIN: 0486648990
ISBN-13 / EAN: 9780486648996
Binding: Paperback
Product Description:
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.
