Author: David J. Peery
Publisher: Courier Corporation
ISBN: 0486485803
Category : Science
Languages : en
Pages : 578
Book Description
"Still relevant 62 years after its initial publication, this legendary reference text on aircraft stress analysis is considered the best book on the subject. A knowledge of aerodynamics is a prerequisite for its discussions of basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition"--
Aircraft Structures
Author: David J. Peery
Publisher: Courier Corporation
ISBN: 0486485803
Category : Science
Languages : en
Pages : 578
Book Description
"Still relevant 62 years after its initial publication, this legendary reference text on aircraft stress analysis is considered the best book on the subject. A knowledge of aerodynamics is a prerequisite for its discussions of basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition"--
Publisher: Courier Corporation
ISBN: 0486485803
Category : Science
Languages : en
Pages : 578
Book Description
"Still relevant 62 years after its initial publication, this legendary reference text on aircraft stress analysis is considered the best book on the subject. A knowledge of aerodynamics is a prerequisite for its discussions of basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition"--
Aircraft Structures for Engineering Students
Author: Thomas Henry Gordon Megson
Publisher: Hodder Education
ISBN: 9780713136814
Category : Aeroelasticity
Languages : en
Pages : 0
Book Description
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.
Publisher: Hodder Education
ISBN: 9780713136814
Category : Aeroelasticity
Languages : en
Pages : 0
Book Description
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.
Airplane Structures
Author: United States. War Department
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 434
Book Description
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 434
Book Description
Airplane Structures
Author: United States. Bureau of Naval Personnel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 176
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 176
Book Description
Airframe Structural Design
Author: Chunyun Niu
Publisher: Adaso Adastra Engineering Center
ISBN: 9789627128090
Category : Airframes
Languages : en
Pages : 612
Book Description
Publisher: Adaso Adastra Engineering Center
ISBN: 9789627128090
Category : Airframes
Languages : en
Pages : 612
Book Description
Composite Materials for Aircraft Structures
Author: Alan A. Baker
Publisher: AIAA
ISBN: 9781600860409
Category : Airplanes
Languages : en
Pages : 626
Book Description
Publisher: AIAA
ISBN: 9781600860409
Category : Airplanes
Languages : en
Pages : 626
Book Description
Understanding Aircraft Structures
Author: John Cutler
Publisher: Grafton Books
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 184
Book Description
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.
Publisher: Grafton Books
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 184
Book Description
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.
Analysis and Design of Flight Vehicle Structures
Author: Elmer Franklin Bruhn
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 1008
Book Description
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 1008
Book Description
Introduction to Aircraft Structural Analysis
Author: T.H.G. Megson
Publisher: Butterworth-Heinemann
ISBN: 1856179338
Category : Technology & Engineering
Languages : en
Pages : 645
Book Description
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
Publisher: Butterworth-Heinemann
ISBN: 1856179338
Category : Technology & Engineering
Languages : en
Pages : 645
Book Description
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
Bonded Repair of Aircraft Structures
Author: A. Baker
Publisher: Springer Science & Business Media
ISBN: 9789024736065
Category : Technology & Engineering
Languages : en
Pages : 236
Book Description
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.
Publisher: Springer Science & Business Media
ISBN: 9789024736065
Category : Technology & Engineering
Languages : en
Pages : 236
Book Description
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.