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Author : Ernest Edwin Sechler,Louis Gerhardus Dunn
Publisher : Unknown
Page : 444 pages
File Size : 45,7 Mb
Release : 1963
Category : Aircraft drafting
ISBN : UOM:39076006543230
Author : Anonim
Publisher : Watchmaker Publishing
Page : 336 pages
File Size : 44,6 Mb
Release : 2005-02
Category : Science
ISBN : 1929148461
Author : Anonim
Publisher : Unknown
Page : 344 pages
File Size : 55,8 Mb
Release : 1920
Category : Electronic
ISBN : 8210379456XXX
Author : Ernest E. Sechler,Louis G. Dunn
Publisher : Unknown
Page : 420 pages
File Size : 50,9 Mb
Release : 1952
Category : Electronic
ISBN : OCLC:631664936
Author : Elmer Franklin Bruhn
Publisher : Unknown
Page : 1008 pages
File Size : 55,7 Mb
Release : 1973
Category : Aeroelasticity
ISBN : UOM:39015037499350
Author : T.H.G. Megson
Publisher : Butterworth-Heinemann
Page : 910 pages
File Size : 42,5 Mb
Release : 2016-10-17
Category : Technology & Engineering
ISBN : 9780081009987
Aircraft Structures for Engineering Students, Sixth Edition, is the leading self-contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its sixth edition, the author has expanded the book’s coverage of analysis and design of composite materials for use in aircraft, and has added new, real-world and design-based examples, along with new end-of-chapter problems of varying complexity. Expanded coverage of composite materials and structures New practical and design-based examples and problems throughout the text aid understanding and relate concepts to real world applications Updated and additional Matlab examples and exercises support use of computational tools in analysis and design Available online teaching and learning tools include downloadable Matlab code, solutions manual, and image bank of figures from the book
Author : Elmer Franklin Bruhn
Publisher : Unknown
Page : 550 pages
File Size : 41,9 Mb
Release : 1949
Category : Airplanes
ISBN : UOM:39015012660091
Author : Denis Howe
Publisher : John Wiley & Sons
Page : 632 pages
File Size : 41,9 Mb
Release : 2004
Category : Science
ISBN : UOM:39015060065136
In this latest contribution to the conceptual design of an aircraft Denis Howe presents comprehensive coverage of all aspects of loading action analysis, together with the logical extension to the conceptual design of the airframe. He thereby meets two perceived needs which are not currently addressed by existing aircraft design texts, where loading analysis tends to be dealt with somewhat superficially, treating only the basic symmetric flight envelope, and where structural analysis often assumes that a certain level of design detail has already been established. Graduate and post-graduate level aeronautical students will welcome the approach offered by Aircraft Loading and Structural Layout. Practising engineers in the aircraft industry will find a useful loading action reference, providing a simple method for the derivation of initial structural data for input to advance analysis programs and the interpretation of the output from them.
Author : Howard D. Curtis
Publisher : McGraw-Hill Science, Engineering & Mathematics
Page : 822 pages
File Size : 55,5 Mb
Release : 1997
Category : Technology & Engineering
ISBN : UOM:39015058332878
The author uses practical applications and real aerospace situations to illustrate concepts in the text covering modern topics including landing gear analysis, tapered beams, cutouts and composite materials. Chapters are included on statically determinate and statically indeterminate structures to serve as a review of material previously learned. Each chapter in the book contains methods and analysis, examples illustrating methods and homework problems for each topic.
Author : Thomas Henry Gordon Megson
Publisher : Hodder Education
Page : 0 pages
File Size : 55,5 Mb
Release : 1990
Category : Aeroelasticity
ISBN : 0713136812
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 : T.H.G. Megson
Publisher : Butterworth-Heinemann
Page : 758 pages
File Size : 48,6 Mb
Release : 2017-06-14
Category : Technology & Engineering
ISBN : 9780081021002
Introduction to Aircraft Structure Analysis, Third Edition covers the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work set 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. As a self-contained guide, this value-priced book is an excellent resource for anyone learning the subject. Based on the author's best-selling text, Aircraft Structures for Engineering Students Contains expanded coverage of composite materials and structures“/li> Includes new practical and design-based examples and problems throughout the text Provides an online teaching and learning tool with downloadable MATLAB code, a solutions manual, and an image bank of figures from the book
Author : Egbert Torenbeek
Publisher : John Wiley & Sons
Page : 412 pages
File Size : 41,9 Mb
Release : 2013-05-28
Category : Technology & Engineering
ISBN : 9781118568095
Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to “what if” questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimization Provides an overview of advanced technologies for propulsion and reducing aerodynamic drag Offers insight into the derivation of design sensitivity information Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts.
Author : Bruce K. Donaldson
Publisher : Unknown
Page : 935 pages
File Size : 55,8 Mb
Release : 1993
Category : Airframes
ISBN : 0071125914
Author : Chunyun Niu,Chʻun-yün Niu
Publisher : Unknown
Page : 632 pages
File Size : 40,9 Mb
Release : 1988
Category : Airframes
ISBN : UVA:X001433308
Author : Bruce K. Donaldson
Publisher : Cambridge University Press
Page : 15 pages
File Size : 43,5 Mb
Release : 2008-03-24
Category : Technology & Engineering
ISBN : 9781107394179
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.