نویسنده: Michael C. Y. Niu

مشخصات: Technical Book Company | May 2005 | ISBN : 9627128082 | PDF Format, 811 pages | English

توضیحات:

Michael Niu has once again produced a very reasonable book. This book is destined to become a standard reference and will complement the other classic in the industry very well (Bruhn's Analysis and Design of Flight Vehicle Structures). The book covers just about most topics required to perform effective practical stress analysis. Again as with Bruhn this is a bit of a cookbook, but in many instances that's what is required to design practical aerospace structures.
Some of the material is a repeat of what's available in Bruhn; however, there is plenty of additional material which makes this book worth having. The big drawback of this book is that there are a lot of mistakes in the formulas, etc.
This was likely a result of trying to rush the book to print. As pointed out in the other reviews, most of the material in this book needs to be cross referenced with other books of company manuals before being used. Having said this the book can still be very useful and one needs to remember that practical stress analysis books are scarce and so Niu is to be congratulated just for trying to put something down on paper.

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نام کتاب: مبانی ایرودینامیک

نویسنده: John D. Anderson

مشخصات: McGraw-Hill Companies | 1991-01-01 | ISBN: 0070016798 | 800 pages | Djvu

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نام کتاب: مبانی دینامیک پرواز

مشخصات: ISBN: 0750669276 | 491 pages | PDF

نام کتاب: مبانی آیرودینامیک (ایرودینامیک) - ويرايش سوم

بها در آمازون: $153 - ۱۵۳ دلار

نویسنده: John D. Anderson

مشخصات: McGraw-Hill Science/Engineering/Math; 3 edition | 2001-01-02| 912 pages | PDF

توضیحات:

* 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

نام کتاب: مسائل پیشرفته طراحی در مهندسی هوافضا - جلد اول: سیستم های پیشرفته هوافضا

نویسنده: Angelo, Ed. Miele

مشخصات: Kluwer Academic/ Plenum Publishers; 1 edition (2004) | 192 pages | PDF | 12,3 Mb

توضیحات:

Advanced Design Problems in Aerospace Engineering, Volume 1: Advanced Aerospace Systems presents six authoritative lectures on the use of mathematics in the conceptual design of various types of aircraft and spacecraft. It covers the following topics: design of rocket-powered orbital spacecraft (Miele/Mancuso), design of Moon missions (Miele/Mancuso), design of Mars missions (Miele/Wang), design of an experimental guidance system with a perspective flight path display (Sachs), neighboring vehicle design for a two-stage launch vehicle (Well), and controller design for a flexible aircraft (Hanel/Well). This is a reference book of interest to engineers and scientists working in aerospace engineering and related topics.

نام کتاب: توربولانس (اشفتگی) جوی (هوایی) : از منظر دینامیک مولکولی

نویسنده: Adrian Tuck

مشخصات: Oxford University Press, USA | 2008-03-15 | ISBN: 0199236534 | 184 pages | PDF | 1,2 Mb

توضیحات:

This book, authored by a well-known researcher and expositor in meteorology, focuses on the direct link between molecular dynamics, turbulence theory, fluid mechanics and non equilibrium statistical mechanics, it is relevant to the fields of applied mathematics, physics and atmospheric
sciences, and focuses on fluid flow and turbulence, as well as on temperature, radiative transfer and chemistry. With extensive references and glossary, this is an ideal text for graduates and researchers in meteorology, applied mathematics and physical chemistry.

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نام کتاب: ایرودینامیک موشک

نویسنده: Jack N. Nielsen

مشخصات: Published by AIAA, © 1988, 450 pages / University Microfilms International Ann Arbor, Michigan USA

The "Bible" of missile aerodynamics

توضیحات: این کتاب از کتب مرجع معرفی شده توسط AIAA در رابطه با منابع آیرودینامیک کاربردی میباشد

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.

Table of Contents:

Introduction
Formulas Commonly Used in Missile Aerodynamics
Slender-Body Theory at Supersonic and Subsonic Speeds
Aerodynamics of Bodies
Vortices
Wing-Body Interference
Downwash, Sidewash, and the Wake
Wing-Tail Interference
Aerodynamic Controls
Drag
Stability Derivatives

نام کتاب: ایرودینامیک ایروالاستیسیتی ایروکاوستیس در توربو ماشین ها

مشخصات: Springer | ISBN:9781402042676 | Edition 2006 | PDF | 626 Pages | 14.5 MB

توضیحات:

This textbook is a collection of technical papers that were presented at the 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines held September 8-11, 2003 at Duke University in Durham, North Carolina. The papers represent the latest in state of the art research in the areas of aeroacoustics, aerothermodynamics, computational methods, experimental testing related to flow instabilities, flutter, forced response, multistage, and rotor-stator effects for turbomachinery.
From the contents:

Foreword.
Preface.
Part 1: Flutter.
Part 2: Forced response.
Part 3: Multistage Effects.
Part 4: Aeroacoustics.
Part 5: Flow instabilities.
Part 6: Computational techniques.
Part 7: Experimental unsteady aerodynamics.
Part 8: Aerothermodynamics.

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نام کتاب: ساخت نیروی هوایی استراتژیک

نویسنده: Walton S Moody

مشخصات: Publisher: US Government Printing Office | 537 pages | PDF | 46 MB

توضیحات:

This authoritative official history deals with the early years of the Air Force's effort to build and maintain a strategic striking force, from 1945 through 1953. It discusses the period of reorganization in national defense in the years after the end of the Second World War, as the Army Air Forces dealt with questions of structure, doctrine, strategy, atomic weapons, and technology

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نام کتاب: Exploring the Secrets of the Aurora

نام کتاب: کاوش در کشف اسرار آئورا

مشخصات: Springer; 1 edition | 246 pages | August 31, 2002 | DJVU

توضیحات:

Prominent progress in science is inevitably associated with controversies. Thus, young researchers, in particular, have to learn how to persevere during the period of controversy and struggle for acceptance. Unfortunately, the skills needed are not taught in textbooks or monographs, which mostly describe the consensus of contemporary experts. This book, which is based on my own experiences as a scientist, describes the history of the progress made in auroral science and magnetospheric physics by providing examples of ideas, controversies, struggles, acceptance, and success in some instances. Although no general methodology (if any exists) is mentioned, I hope that the reader will learn about the history of progress in auroral science and examples (right or wrong) of dealing with the controversies.

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نام کتاب: تئوری و طراحی ایرکاشن

مشخصات: Publisher: Butterworth-Heinemann/Publication Date: 2000-05-26/Number Of Pages: 632

توضیحات:

This definitive text describes the theory and design both of Air Cushion Vehicles (ACV) and Surface Effect Ships (SES). It begins by introducing hovercraft types and their development and application throughout the world in the last three decades, before going on to discuss the theoretical aspects of ACV and SES craft covering their hovering performance, dynamic trim over calm water, resistance, stability, manoeuvrability, skirt configuration and analysis of forces acting on the skirts, ACV and SES seakeeping, and the methodology of scaling aerodynamic and hydrodynamic forces acting on the ACV/SES from model test data. The latter chapters describe a design methodology, including design criteria and standard methods for estimating craft performance, lift system design, skirt design, hull structure, propulsion systems and power unit selection. Much technical information, data, and references to further work on hovercraft and SES design is provided. The book will be a useful reference to engineers, technicians, teachers, students (both undergraduate and postgraduate), operators etc. who are involved in ACV/SES research, design, construction and operation.

Audience
Postgraduates and professionals in marine engineering. Hovercraft enthusiasts.

Contents
Introduction to hovercraft * Air cushion theory * Steady drag forces * Stability * Trim and water surface deformation under the cushion * Manoeuvrability * Design and analysis of ACV and SES skirts * Motions in waves * Model experiments and scaling laws * Design methodology and performance estimation * Determination of principal dimensions of ACV*SES * Lift system design * Skirt design * Structural design * Propulsion system design * Power unit selection.

نام کتاب: تحلیل واکنش فضا پیما و سازه های هوایی به توربولانس (آشفتی) جوی

نویسنده: Willem Van Staveren

مشخصات: Delft Univ Pr | 2003-12 | ISBN:9040724539 | 502 pages | PDF

توضیحات:

This is a Ph.D. dissertation. The response of aircraft to stochastic atmospheric turbulence plays an important role in, for example, aircraft design (load calculations) and flight simulation (handling qualities research and pilot training). In order to simulate these aircraft responses, an accurate mathematical model is required. Two classical models will be discussed in this thesis that is the Delft University of Technology (DUT) model and the Four Point Aircraft (FPA) model. Although they are well established, their fidelity remains obscure. The cause lies in one of the requirements for system identification; it has always been necessary to relate inputs to outputs to determine, or identify, system dynamic characteristics. From experiments, using both the measured input and the measured output, a mathematical model of any system can be obtained.

When considering an input-output system such as an aircraft subjected to stochastic atmospheric turbulence, a major problem emerges. During flight tests, no practical difficulty arises measuring the aircraft-system's outputs, such as the angle-of-attack, the pitch-angle, the roll-angle, etc. However, a huge problem arises when the input to the aircraft-system is considered; this input is stochastic atmospheric turbulence in this thesis. Currently, it still remains extremely difficult to identify the entire flowfield around an aircraft's geometry subjected to a turbulent field of flow; an infinite amount of sensors would be required to identify the atmospheric turbulence velocity component's distribution (the input) over it. As a consequence, it is difficult, if not impossible, to identify atmospheric turbulence models from flight tests.

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نام کتاب: ساختار و ساختمان فضاپیماها برای دانشجویان مهندسی - ویرایش سوم

نویسنده: T. H. G. Megson, Department of Civil Engineering, Leeds University, UK

توضیحات:

'This is an excellent book and should find a place on the shelf of any student or practising engineer involved in aircraft structural analysis. I can recommend it to the aeronautical community without reservation'The Aeronautical Journal, October 2001 (Prof. A.J. Morris) As an introduction to the problems encountered in the structural design of modern aircraft, Megson's book can be recommended to both students and those engaged in structural analysis aerospace design offices