Author : David J. Peery
Publisher : Courier Corporation
Page : 578 pages
File Size : 35,18 MB
Release : 2013-04-29
Category : Science
ISBN : 048626730X
This legendary, still-relevant reference text on aircraft stress analysis discusses basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition.
Author : Thomas Henry Gordon Megson
Publisher : Hodder Education
Page : 0 pages
File Size : 19,81 MB
Release : 1990
Category : Aeroelasticity
ISBN : 9780713136814
This book provides a self-contained course in aircraft structures which contains not only the fundamentals of elasticity and aircraft structural analysis but also the associated topics of airworthiness and aeroelasticity.
Author : Bruce K. Donaldson
Publisher : Cambridge University Press
Page : 15 pages
File Size : 40,2 MB
Release : 2008-03-24
Category : Technology & Engineering
ISBN : 1107394171
As with the first edition, this textbook provides a clear introduction to the fundamental theory of structural analysis as applied to vehicular structures such as aircraft, spacecraft, automobiles and ships. The emphasis is on the application of fundamental concepts of structural analysis that are employed in everyday engineering practice. All approximations are accompanied by a full explanation of their validity. In this new edition, more topics, figures, examples and exercises have been added. There is also a greater emphasis on the finite element method of analysis. Clarity remains the hallmark of this text and it employs three strategies to achieve clarity of presentation: essential introductory topics are covered, all approximations are fully explained and many important concepts are repeated.
Author : United States. War Department
Publisher :
Page : 434 pages
File Size : 31,35 MB
Release : 1941
Category : Airframes
ISBN :
Author : John Cutler
Publisher : Grafton Books
Page : 184 pages
File Size : 32,28 MB
Release : 1981
Category : Technology & Engineering
ISBN :
This book explains aircraft structures so as to provide a basic understanding of the subject and the terminology used, as well as illustrating some of the problems.It provides a brief historical background, and covers parts of the aeroplane, loads, structural form, materials, processes, detail design, quality control, stressing, and the documentation associated with modification and repairs.The Fourth Edition takes account of new materials and the new European regulatory system.
Author : Elmer Franklin Bruhn
Publisher :
Page : 1008 pages
File Size : 40,38 MB
Release : 1973
Category : Aeroelasticity
ISBN :
Author : United States. Bureau of Naval Personnel
Publisher :
Page : 176 pages
File Size : 16,83 MB
Release : 1945
Category : Airplanes
ISBN :
Author : A. Baker
Publisher : Springer Science & Business Media
Page : 236 pages
File Size : 29,34 MB
Release : 1988-05-31
Category : Technology & Engineering
ISBN : 9789024736065
The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability.
Author : T.H.G. Megson
Publisher : Butterworth-Heinemann
Page : 645 pages
File Size : 35,89 MB
Release : 2010-01-16
Category : Technology & Engineering
ISBN : 1856179338
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
Author : Rhys Jones
Publisher : Butterworth-Heinemann
Page : 972 pages
File Size : 22,49 MB
Release : 2017-12-05
Category : Technology & Engineering
ISBN : 008100544X
Aircraft Sustainment and Repair is a one-stop-shop for practitioners and researchers in the field of aircraft sustainment, adhesively bonded aircraft joints, bonded composites repairs, and the application of cold spray to military and civil aircraft. Outlining the state-of-the-art in aircraft sustainment, this book covers the use of quantitative fractography to determine the in-service crack length versus flight hours curve, the effect of intergranular cracking on structural integrity and the structural significance of corrosion. The book additionally illustrates the potential of composite repairs and SPD applications to metallic airframes. Covers corrosion damage assessment and management in aircraft structures Includes a key chapter on U.S. developments in the emerging field of supersonic particle deposition (SPD) Shows how to design and assess the potential benefits of both bonded composite repairs and SPD repairs to metallic aircraft structures to meet the damage tolerance requirements inherent in FAA ac 20-107b and the U.S. Joint Services
