Author : David J. Peery
Publisher : Courier Corporation
Page : 578 pages
File Size : 40,69 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 : 24,26 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 : John Cutler
Publisher : Grafton Books
Page : 184 pages
File Size : 44,27 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 : Bruce K. Donaldson
Publisher : Cambridge University Press
Page : 15 pages
File Size : 23,37 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 : 23,7 MB
Release : 1941
Category : Airframes
ISBN :
Author : United States. Bureau of Naval Personnel
Publisher :
Page : 176 pages
File Size : 22,40 MB
Release : 1945
Category : Airplanes
ISBN :
Author : Elmer Franklin Bruhn
Publisher :
Page : 1008 pages
File Size : 42,18 MB
Release : 1973
Category : Aeroelasticity
ISBN :
Author : Chunyun Niu
Publisher : Adaso Adastra Engineering Center
Page : 612 pages
File Size : 13,57 MB
Release : 1999
Category : Airframes
ISBN : 9789627128090
Author : Alan A. Baker
Publisher : AIAA
Page : 626 pages
File Size : 50,9 MB
Release : 2004
Category : Airplanes
ISBN : 9781600860409
Author : Rhys Jones
Publisher : Butterworth-Heinemann
Page : 972 pages
File Size : 42,15 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
