Practical Analysis of Aircraft Composites
| Author | : Brian Esp |
| Publisher | : |
| Total Pages | : |
| Release | : 2017-10-28 |
| Genre | : |
| ISBN | : 9780983245391 |
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Composite Materials for Aircraft Structures
| Author | : Alan A. Baker |
| Publisher | : AIAA |
| Total Pages | : 626 |
| Release | : 2004 |
| Genre | : Airplanes |
| ISBN | : 9781600860409 |
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Composite Materials in Aerospace Design
| Author | : G.I. Zagainov |
| Publisher | : Springer Science & Business Media |
| Total Pages | : 474 |
| Release | : 1996 |
| Genre | : Gardening |
| ISBN | : 9780412584701 |
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Composite Materials in Aerospace Design is one of six titles in a coherent and definitive series dedicated to advanced composite materials research, development and usage in the former Soviet Union. Much of the information presented has been classified until recently. Thus each volume provides a unique insight into hitherto unknown research and development data. This volume deals with the design philosophy and methodology used to produce primary and secondary load bearing composite structures with high life expectancies. The underlying theme is of extensive advanced composites research and development programs in aircraft and spacecraft applications, including the space orbital ship `BURAN'. The applicability of much of this work to other market sectors, such as automotive, shipbuilding and sporting goods is also examined in some detail. The text starts by describing typical structures for which composites may be used in this area and some of the basic requirements from the materials being used. Design of components with composite materials is then discussed, with specific reference to case studies. This is followed by discussion and results from evaluation of finished structures and components, methods of joining with conventional materials and finally, non-destructive testing methods and forecasting of the performance of the composite materials and the structures which they form. Composite Materials in Aerospace Design will be of interest to anyone researching or developing in composite materials science and technology, as well as design and aerospace engineers, both in industry and universities.
Aircraft Materials and Analysis
| Author | : Tariq Siddiqui |
| Publisher | : McGraw Hill Professional |
| Total Pages | : 289 |
| Release | : 2014-12-06 |
| Genre | : Transportation |
| ISBN | : 0071831142 |
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Complete coverage of aircraft design, manufacturing, and maintenance Aircraft Materials and Analysis addresses aircraft design, mechanical and structural factors in aviation, flight loads, structural integrity, stresses, properties of materials, compression, bending, and aircraft fatigue. Detailed analysis of the failure process is provided. This authoritative guide examines materials used in aircraft construction such as aluminum, steel, glass, composite, rubber, and carbon fiber. Maintenance procedures for corrosion and aging aircraft are discussed and methods of inspection such as nondestructive testing and nondestructive inspection are described. Accident investigation case studies review aircraft design, material behavior, NTSB findings, safety, stress factors, and human factor involvement. End-of-chapter questions reinforce the topics covered in this practical resource. Aircraft Materials and Analysis covers: The aircraft--standards for design, structural integrity, and system safety Aircraft materials Loads on the aircraft Stress analysis Torsion, compression, and bending loads Aircraft riveted joints and pressure vessels Heat treatments of metals Aircraft fatigue/aircraft material fatigue Aircraft corrosion Dynamic stress, temperature stress, and experimental methods Composites Nondestructive Testing (NDT) Aviation maintenance management Case studies and human factors
Practical Analysis of Composite Laminates
| Author | : J. N. Reddy |
| Publisher | : CRC Press |
| Total Pages | : 209 |
| Release | : 2018-02-06 |
| Genre | : Technology & Engineering |
| ISBN | : 1351423045 |
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Composite materials are increasingly used in aerospace, underwater, and automotive structures. They provide unique advantages over their metallic counterparts, but also create complex challenges to analysts and designers. Practical Analysis of Composite Laminates presents a summary of the equations governing composite laminates and provides practical methods for analyzing most common types of composite structural elements. Experimental results for several types of structures are included, and theoretical and experimental correlations are discussed. The last chapter is devoted to practical analysis using Designing Advanced Composites (DAC), a PC-based software on the subject. This comprehensive text can be used for a graduate course in mechanical engineering, and as a valuable reference for professionals in the field.
Design and Analysis of Composite Structures
| Author | : Christos Kassapoglou |
| Publisher | : John Wiley & Sons |
| Total Pages | : 303 |
| Release | : 2011-07-05 |
| Genre | : Technology & Engineering |
| ISBN | : 1119957060 |
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Design and Analysis of Composite Structures enables graduate students and engineers to generate meaningful and robust designs of complex composite structures. Combining analysis and design methods for structural components, the book begins with simple topics such as skins and stiffeners and progresses through to entire components of fuselages and wings. Starting with basic mathematical derivation followed by simplifications used in real-world design, Design and Analysis of Composite Structures presents the level of accuracy and range of applicability of each method. Examples taken from actual applications are worked out in detail to show how the concepts are applied, solving the same design problem with different methods based on different drivers (e.g. cost or weight) to show how the final configuration changes as the requirements and approach change. Provides a toolkit of analysis and design methods to most situations encountered in practice, as well as analytical frameworks and the means to solving them for tackling less frequent problems. Presents solutions applicable to optimization schemes without having to run finite element models at each iteration, speeding up the design process and allowing examination of several more alternatives than traditional approaches. Includes guidelines showing how decisions based on manufacturing considerations affect weight and how weight optimization may adversely affect the cost. Accompanied by a website at www.wiley.com/go/kassapoglou hosting lecture slides and solutions to the exercises for instructors.
Practical Stress Analysis for Design Engineers
| Author | : Jean-Claude Flabel |
| Publisher | : |
| Total Pages | : 685 |
| Release | : 1997-01-01 |
| Genre | : Technology & Engineering |
| ISBN | : 9780964701403 |
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Practical Micromechanics of Composite Materials
| Author | : Jacob Aboudi |
| Publisher | : Butterworth-Heinemann |
| Total Pages | : 416 |
| Release | : 2021-08-31 |
| Genre | : Technology & Engineering |
| ISBN | : 0128206381 |
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Practical Micromechanics of Composite Materials provides an accessible treatment of micromechanical theories for the analysis and design of multi-phased composites. Written with both students and practitioners in mind and coupled with a fully functional MATLAB code to enable the solution of technologically relevant micromechanics problems, the book features an array of illustrative example problems and exercises highlighting key concepts and integrating the MATLAB code. The MATLAB scripts and functions empower readers to enhance and create new functionality tailored to their needs, and the book and code highly complement one another. The book presents classical lamination theory and then proceeds to describe how to obtain effective anisotropic properties of a unidirectional composite (ply) via micromechanics and multiscale analysis. Calculation of local fields via mechanical and thermal strain concentration tensors is presented in a unified way across several micromechanics theories. The importance of these local fields is demonstrated through the determination of consistent Margins of Safety (MoS) and failure envelopes for thermal and mechanical loading. Finally, micromechanics-based multiscale progressive damage is discussed and implemented in the accompanying MATLAB code. Emphasizes appropriate application of micromechanics theories to composite behavior Addresses multiple popular micromechanics theories, which are provided in MATLAB Discusses stresses and strains resulting from realistic thermal and mechanical loading Includes availability of solution manual for professors using the book in the classroom
Introduction to Aircraft Structural Analysis
| Author | : T.H.G. Megson |
| Publisher | : Butterworth-Heinemann |
| Total Pages | : 648 |
| Release | : 2010-01-16 |
| Genre | : Technology & Engineering |
| ISBN | : 9781856179331 |
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Introduction to Aircraft Structural Analysis is an essential resource for learning aircraft structural analysis. Based on the author's best-selling book Aircraft Structures for Engineering Students, this brief text introduces the reader to the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work sets the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations. The book covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aero elasticity. It consists of 23 chapters covering a variety of topics from basic elasticity to torsion of solid sections; energy methods; matrix methods; bending of thin plates; structural components of aircraft; airworthiness; airframe loads; bending of open, closed, and thin walled beams; combined open and closed section beams; wing spars and box beams; and fuselage frames and wing ribs. This book will appeal to undergraduate and postgraduate students of aerospace and aeronautical engineering, as well as professional development and training courses. Based on the author's best-selling text Aircraft Structures for Engineering Students, this Intro version covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aeroelasticity Systematic step by step procedures in the worked examples Self-contained, with complete derivations for key equations
Advanced Mechanics of Composite Materials
| Author | : Valery V. Vasiliev |
| Publisher | : Elsevier |
| Total Pages | : 505 |
| Release | : 2007-05-16 |
| Genre | : Technology & Engineering |
| ISBN | : 008048817X |
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Composite materials have been representing most significant breakthroughs in various industrial applications, particularly in aerospace structures, during the past thirty five years. The primary goal of Advanced Mechanics of Composite Materials is the combined presentation of advanced mechanics, manufacturing technology, and analysis of composite materials. This approach lets the engineer take into account the essential mechanical properties of the material itself and special features of practical implementation, including manufacturing technology, experimental results, and design characteristics. Giving complete coverage of the topic: from basics and fundamentals to the advanced analysis including practical design and engineering applications. At the same time including a detailed and comprehensive coverage of the contemporary theoretical models at the micro- and macro- levels of material structure, practical methods and approaches, experimental results, and optimisation of composite material properties and component performance. The authors present the results of more than 30 year practical experience in the field of design and analysis of composite materials and structures. * Eight chapters progressively covering all structural levels of composite materials from their components through elementary plies and layers to laminates* Detailed presentation of advanced mechanics of composite materials * Emphasis on nonlinear material models (elasticity, plasticity, creep) and structural nonlinearity
