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EN-EZEL · 20 فروردین، ۱۳۸۹

Advanced Dynamics - Aiaa Education Series

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

File type: RAR

Size: 3237 KB

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EN-EZEL · 20 فروردین، ۱۳۸۹

Missile Aerodynamics

Missile Aerodynamics

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

PDF

حجم : 19.87 MB

صفحات : 450 صفحه

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EN-EZEL · 20 فروردین، ۱۳۸۹

Basic Helicopter Aerodynamics

Basic Helicopter Aerodynamics: An Account of First Principles in the Fluid Mechanics and Flight Dynamics of the Single Rotor Helicopter

By J. Seddon,&nbspSimon 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

pdf, 8,808kb

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EN-EZEL · 20 فروردین، ۱۳۸۹

Analysis of Low Speed Unsteady Airfoil Flows Analysis of Low Speed Unsteady Airfoil Flows

Author(s): Tuncer Cebeci, Max Platzer, Hsun Chen, Kuo-cheng Chang, Jian P. Shao

Publisher: Springer

Date : 2005

Pages : 230

Format : PDF

OCR : Y

Quality : good

Language : English

ISBN-10 : 3540229329

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EN-EZEL · 20 فروردین، ۱۳۸۹

Computational Fluid Dynamics free download

Author(s): John Anderson

Publisher: McGraw-Hill Science/Engineering/Math

Date : 1995

Pages : 574

Format : djvu

OCR : Y

Quality : good

Language : English

ISBN-10 : 0070016852

ISBN-13 :

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EN-EZEL · 21 فروردین، ۱۳۸۹

Aerodynamics, Aeronautics, and Flight Mechanics

By Barnes W. McCormick

Publisher: Wiley
Number Of Pages: 652
Publication Date: 1994-08-01
ISBN-10 / ASIN: 0471575062
ISBN-13 / EAN: 9780471575061
Binding: Paperback

Product Description:

A New Edition of the Most Effective Text/Reference in the Field! Aerodynamics, Aeronautics, and Flight Mechanics, Second Edition Barnes W. McCormick, Pennsylvania State University 57506-2 When the first edition of Aerodynamics, Aeronautics, and Flight Mechanics was published, it quickly became one of the most important teaching and reference tools in the field. Not only did generations of students learn from it, they continue to use it on the job-the first edition remains one of the most well-thumbed guides you'll find in an airplane company. Now this classic text/reference is available in a bold new edition. All new material and the interweaving of the computer throughout make the Second Edition even more practical and current than before! A New Edition as Complete and Applied as the First Both analytical and applied in nature, Aerodynamics, Aeronautics, and Flight Mechanics presents all necessary derivations to understand basic principles and then applies this material to specific examples. You'll find complete coverage of the full range of topics, from aerodynamics to propulsion to performance to stability and control. Plus, the new Second Edition boasts the same careful integration of concepts that was an acclaimed feature of the previous edition. For example, Chapters 9, 10, and 11 give a fully integrated presentation of static, dynamic, and automatic stability and control. These three chapters form the basis of a complete course on stability and control. New Features You'll Find in the Second Edition

* A new chapter on helicopter and V/STOL aircraft- introduces a phase of aerodynamics not covered in most current texts

* Even more material than the previous edition, including coverage of stealth airplanes and delta wings

* Extensive use of the computer throughout- each chapter now contains several computer exercises

* A computer disk with programs written by the author is available

Only 179 pages of 652

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EN-EZEL · 21 فروردین، ۱۳۸۹

کتاب Airplane Flight Dynamics and Automatic Flight Controls Part II

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EN-EZEL · 21 فروردین، ۱۳۸۹

Aircraft system safety: Military and civil aeronautical applications: Military and Civil Aeronautical Applications

By D E Kritzinger

Publisher: Woodhead Publishing
Number Of Pages: 376
Publication Date: 2006-05-30
ISBN-10 / ASIN: 1845691369
ISBN-13 / EAN: 9781845691363

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EN-EZEL · 21 فروردین، ۱۳۸۹

Stability and Control of Aircraft Systems: Introduction to Classical Feedback Control

Stability and Control of Aircraft Systems: Introduction to Classical Feedback Control (Aerospace Series (PEP))

By Roy Langton

Publisher: Wiley
Number Of Pages: 254
Publication Date: 2006-11-17
ISBN-10 / ASIN: 0470018917
ISBN-13 / EAN: 9780470018910
Binding: Hardcover

Product Description:

In the current climate of increasing complexity and functional integration in all areas of engineering and technology, stability and control are becoming essential ingredients of engineering knowledge. Many of todayâ€™s products contain multiple engineering technologies, and what were once simple mechanical, hydraulic or pneumatic products now contain integrated electronics and sensors. Control theory reduces these widely varied technical components into their important dynamic characteristics, expressed as transfer functions, from which the subtleties of dynamic behaviours can be analyzed and understood.

Stability and Control of Aircraft Systems is an easy-to-read and understand text that describes control theory using minimal mathematics. It focuses on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples.

Clarifies the design and development of feedback control systems
Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background
Illustrated throughout with figures and tables

Stability and Control of Aircraft Systems provides both the seasoned engineer and the graduate with the know-how necessary to minimize problems with fielded systems in the area of operational performance

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EN-EZEL · 21 فروردین، ۱۳۸۹

Aviation Safety and Pilot Control

Aviation Safety and Pilot Control: Understanding and Preventing Unfavorable Pilot/Vehicle Interactions

By Committee on the Effects of Aircraft-Pilot Coupling on Flight Safety, National Research Council

* Publisher: National Academies Press

* Number Of Pages: 220

* Publication Date: 1997-02-28

* ISBN-10 / ASIN: 0309056888

* ISBN-13 / EAN: 9780309056885

Book Description:

Adverse aircraft-pilot coupling (APC) events include a broad set of undesirable and sometimes hazardous phenomena that originate in anomalous interactions between pilots and aircraft. As civil and military aircraft technologies advance, interactions between pilots and aircraft are becoming more complex. Recent accidents and other incidents have been attributed to adverse APC in military aircraft. In addition, APC has been implicated in some civilian incidents.

This book evaluates the current state of knowledge about adverse APC and processes that may be used to eliminate it from military and commercial aircraft. It was written for technical, government, and administrative decisionmakers and their technical and administrative support staffs; key technical managers in the aircraft manufacturing and operational industries; stability and control engineers; aircraft flight control system designers; research specialists in flight control, flying qualities, human factors; and technically knowledgeable lay readers

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EN-EZEL · 21 فروردین، ۱۳۸۹

Airplane Performance, Stability and Control

By Courtland D. Perkins, Robert E. Hage

* Publisher: Wiley

* Number Of Pages: 504

* Publication Date: 1949-01-01

* ISBN-10 / ASIN: 047168046X

* ISBN-13 / EAN: 9780471680468

Given that you understand differential calculus (not just Calculus 1), this is an excellent book for the professional and the serious amateur aircraft maker. This is a far better book than Perkin's second book on Stability and Control. That tome is both pompous and difficult to understand. Unlike his second book this book is written in a straightforward and very easy to understand manner. Therein lies the reason that this book has been a standard reference for 50 years.

23.43 MB

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EN-EZEL · 21 فروردین، ۱۳۸۹

Strapdown Inertial Navigation Technology

(IEE Radar, Sonar, Navigation and Avionics Series)

By David Titterton , John Weston

* Publisher: IEE

* Number Of Pages: 558

* Publication Date: 2005-01-01

* ISBN-10 / ASIN: 0863413587

* ISBN-13 / EAN: 9780863413582

Product Description:

Inertial navigation is widely used for the guidance of aircraft, missiles ships and land vehicles, as well as in a number of novel applications such as surveying underground pipelines in drilling operations. This book sets out to provide a clear and concise description of the physical principles of inertial navigation, the associated growth of errors and their compensation. There is also detailed treatment of recent developments in inertial sensor technology and a description of techniques for implementing and evaluating such systems. This new edition includes a number of refinements covering sensor technology, geodesy and error modelling, the major additions to the original text are new chapters on MEMS technology and intertial system applications

27342 KB

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EN-EZEL · 21 فروردین، ۱۳۸۹

Modeling and Simulation of Aerospace Vehicle Dynamics

Modeling and Simulation of Aerospace Vehicle Dynamics (Aiaa Education Series)

By Peter H. Zipfel

* Publisher: AIAA (American Institute of Aeronautics & Ast

* Number Of Pages: 567

* Publication Date: 2007-04-15

* ISBN-10 / ASIN: 1563478757

* ISBN-13 / EAN: 9781563478758

Book Description:

This book unifies all aspects of flight dynamics for the efficient development of aerospace vehicle simulations. It provides the reader with a complete set of tools to build, program, and execute simulations. Unlike other books, it uses tensors for modeling flight dynamics in a form invariant under coordinate transformations. For implementation, the tensors are converted to matrices, resulting in compact computer code. The reader can pick templates of missiles, aircraft, or hypersonic vehicles to jump-start a particular application.

It is the only textbook that combines the theory of modeling with hands-on examples of three-, five-, and six-DoF simulations. Free access to eight prototype simulations and to CADAC Studio–used in the United States, United Kingdom, France, and Germany–is included with the book.

Amply illustrated with 318 figures and 44 examples, the text can be used for advanced undergraduate and graduate instruction or for self-study. Also included are 77 problems that enhance the ability to model aerospace vehicles and nine projects that hone the skills for developing three-, five-, and six-DoF simulations. Instructors may request a solution manual at no cost from the publisher.

Rar'd PDF files

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28098 KB

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EN-EZEL · 21 فروردین، ۱۳۸۹

Flight Stability and Automatic Control

By Robert C. Nelson

* Publisher: Mcgraw-Hill College

* Number Of Pages: 286

* Publication Date: 1989-03

* ISBN-10 / ASIN: 0070462186

* ISBN-13 / EAN: 9780070462182

If this is a required text, as it was for me then buy it. The information isnt bad, and gives a good coverage of the subject, but the errata list I receieved from my professor spanned at least 20 pages, front and back. You'll learn controls with the right professor, but expect the book to confuse you with changing subscripts, even changing values in example problems. For example, the area of a wing in one example problem is listed as 945 ft^2 and yet the problem solves using the area of 965 ft^2. Equations will be missing subscripts entirely, or duplicate them. For example, in one end of the chapter section of problems, the 2-D coefficient of lift for the tail is listed twice as opposed to giving you one value for the tail, and another for the wing as they should have. Expect to make assumptions like they have never been made before either. So much will not be given to you, it will be up to you to decide what value is reasonable that youll use. Good luck to you if this is a required text

9.75MB

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EN-EZEL · 21 فروردین، ۱۳۸۹

Aircraft Dynamics and Automatic Control

By Duane McRuer, Dunstan Graham, Irving Ashkenas

* Publisher: Princeton Univ Pr

* Number Of Pages: 809

* Publication Date: 1973-01-01

* ISBN-10 / ASIN: 0691080836

* ISBN-13 / EAN: 9780691080833

Book Description:

Aeronautical engineers concerned with the analysis of aircraft dynamics and the synthesis of aircraft flight control systems will find an indispensable tool in this analytical treatment of the subject. Approaching these two fields with the conviction that an understanding of either one can illuminate the other, the authors have summarized selected, interconnected techniques that facilitate a high level of insight into the essence of complex systems problems. These techniques are suitable for establishing nominal system designs, for forecasting off-nominal problems, and for diagnosing the root causes of problems that almost inevitably occur in the design process. A complete and self-contained work, the text discusses the early history of aircraft dynamics and control, mathematical models of linear system elements, feedback system analysis, vehicle equations of motion, longitudinal and lateral dynamics, and elementary longitudinal and lateral feedback control. The discussion concludes with such topics as the system design process, inputs and system performance assessment, and multi-loop flight control systems.

PDF = 24.34 MB

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EN-EZEL · 21 فروردین، ۱۳۸۹

Radar And Laser Cross Section Engineering

(Aiaa Education Series)

By David C. Jenn

* Publisher: AIAA (American Institute of Aeronautics & Ast

* Number Of Pages: 505

* Publication Date: 2005-08-20

* ISBN-10 / ASIN: 1563477025

* ISBN-13 / EAN: 9781563477027

Book Description:

Prediction, reduction, and measurement of electromagnetic scattering from complex three-dimensional targets are the primary emphasis of this text, developed by the author from courses taught at the Naval Postgraduate School. The analysis methods discussed focus on physical optics and numerical solutions to Maxwell's equations (the method of moments and finite-difference solutions) as they apply to radar cross section. Numerous examples have been included to illustrate the application of important methods and concepts.

Written as an instructional text, this book is recommended for upper-level undergraduate and graduate students. Also a good reference book for engineers in industry

8058 KB

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EN-EZEL · 21 فروردین، ۱۳۸۹

Commercial Aviation Safety

By Alexander T. Wells

* Publisher: McGraw-Hill Professional Publishing

* Number Of Pages: 436

* Publication Date: 2001-04-19

* ISBN-10 / ASIN: 0071374108

* ISBN-13 / EAN: 9780071374101

Book Description:

*An overview of airline industry safety statistics, standards, and mandates

*Covers FAA regulatory structure, development of technologies, management roles, air transport safety measurement methods - and more

*Includes tables relating to commercial aviation accident statistics

*New chapter on Aviation Security

2.02 MB ~ Rar'd PDF

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EN-EZEL · 21 فروردین، ۱۳۸۹

Controlling Pilot Error: Controlled Flight Into Terrain (CFIT/CFTT

Controlling Pilot Error: Controlled Flight Into Terrain (CFIT/CFTT)

By Daryl R. Smith

* Publisher: McGraw-Hill Professional

* Number Of Pages: 352

* Publication Date: 2001-06-08

* ISBN-10 / ASIN: 0071374116

* ISBN-13 / EAN: 9780071374118

Book Description:

With up to 80% of accidents attributed to pilot error, this new series is critically important. It identifies and examines the ten top areas of concern to pilot safety. Each book contains real-life pilot stories drawn from FAA/NASA databases, valuable "save-yourself" techniques and an action agenda of preventive techniques pilots can implement to avoid risks.

Rar'd PDF

1.21 MB

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EN-EZEL · 21 فروردین، ۱۳۸۹

Introduction to Aircraft Performance, Selection and Design

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Introduction to Aircraft Performance, Selection and Design

By Francis J. Hale

Publisher: Wiley

Number Of Pages: 336

Publication Date: 1984-03

ISBN / ASIN: 0471078859

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EN-EZEL · 21 فروردین، ۱۳۸۹

Fundamentals of Airplane Flight Mechanics

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Fundamentals of Airplane Flight Mechanics

By David G. Hull

Publisher: Springer

Number Of Pages: 298

Publication Date: 2007-03

ISBN / ASIN: 3540465715

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