Thermal Structures for Aerospace Applications
Author: Earl Arthur Thornton
Publisher: AIAA
Published: 1996
Total Pages: 508
ISBN-13: 9781600861260
DOWNLOAD EBOOKRead and Download eBook Full
Author: Earl Arthur Thornton
Publisher: AIAA
Published: 1996
Total Pages: 508
ISBN-13: 9781600861260
DOWNLOAD EBOOKAuthor: Elmer Franklin Bruhn
Publisher:
Published: 1973
Total Pages: 1008
ISBN-13:
DOWNLOAD EBOOKAuthor: D. J. Johns
Publisher: Elsevier
Published: 2013-10-22
Total Pages: 230
ISBN-13: 1483227049
DOWNLOAD EBOOKThermal Stress Analyses deals with both elastic and plastic thermal stresses produced from large variations in temperature and thermal expansion in materials whose properties are time-independent. This book is composed of eight chapters. The opening chapter illustrates the general three-dimensional thermoelastic problem, which requires the determination of stress, strains and displacements, when the body forces and boundary conditions are known while the next chapter demonstrate a simpler, two-dimensional formulation involving plane strain and plane stress. The succeeding five chapters describe thermal stresses in various structures, including in thin plates, beams, circular cylinders, and shells. The closing chapters consider the mechanism of thermal buckling and sundry design problems. This book is of value to mechanical engineers, and to mechanical engineering teachers and students.
Author: Erasmo Carrera
Publisher: Academic Press
Published: 2016-11-25
Total Pages: 442
ISBN-13: 0124200931
DOWNLOAD EBOOKThermal Stress Analysis of Composite Beams, Plates and Shells: Computational Modelling and Applications presents classic and advanced thermal stress topics in a cutting-edge review of this critical area, tackling subjects that have little coverage in existing resources. It includes discussions of complex problems, such as multi-layered cases using modern advanced computational and vibrational methods. Authors Carrera and Fazzolari begin with a review of the fundamentals of thermoelasticity and thermal stress analysis relating to advanced structures and the basic mechanics of beams, plates, and shells, making the book a self-contained reference. More challenging topics are then addressed, including anisotropic thermal stress structures, static and dynamic responses of coupled and uncoupled thermoelastic problems, thermal buckling, and post-buckling behavior of thermally loaded structures, and thermal effects on panel flutter phenomena, amongst others. - Provides an overview of critical thermal stress theory and its relation to beams, plates, and shells, from classical concepts to the latest advanced theories - Appeals to those studying thermoelasticity, thermoelastics, stress analysis, multilayered structures, computational methods, buckling, static response, and dynamic response - Includes the authors' unified formulation (UF) theory, along with cutting-edge topics that receive little coverage in other references - Covers metallic and composite structures, including a complete analysis and sample problems of layered structures, considering both mesh and meshless methods - Presents a valuable resource for those working on thermal stress problems in mechanical, civil, and aerospace engineering settings
Author: Tariq Siddiqui
Publisher: McGraw Hill Professional
Published: 2014-12-06
Total Pages: 289
ISBN-13: 0071831142
DOWNLOAD EBOOKComplete 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
Author: O. A. Bauchau
Publisher: Springer Science & Business Media
Published: 2009-08-03
Total Pages: 943
ISBN-13: 9048125162
DOWNLOAD EBOOKThe authors and their colleagues developed this text over many years, teaching undergraduate and graduate courses in structural analysis courses at the Daniel Guggenheim School of Aerospace Engineering of the Georgia Institute of Technology. The emphasis is on clarity and unity in the presentation of basic structural analysis concepts and methods. The equations of linear elasticity and basic constitutive behaviour of isotropic and composite materials are reviewed. The text focuses on the analysis of practical structural components including bars, beams and plates. Particular attention is devoted to the analysis of thin-walled beams under bending shearing and torsion. Advanced topics such as warping, non-uniform torsion, shear deformations, thermal effect and plastic deformations are addressed. A unified treatment of work and energy principles is provided that naturally leads to an examination of approximate analysis methods including an introduction to matrix and finite element methods. This teaching tool based on practical situations and thorough methodology should prove valuable to both lecturers and students of structural analysis in engineering worldwide. This is a textbook for teaching structural analysis of aerospace structures. It can be used for 3rd and 4th year students in aerospace engineering, as well as for 1st and 2nd year graduate students in aerospace and mechanical engineering.
Author: Bruno A. Boley
Publisher: Courier Corporation
Published: 2012-05-23
Total Pages: 610
ISBN-13: 0486143864
DOWNLOAD EBOOKHighly regarded text presents detailed discussion of fundamental aspects of theory, background, problems with detailed solutions. Basics of thermoelasticity, heat transfer theory, thermal stress analysis, more. 1985 edition.
Author:
Publisher:
Published: 1990
Total Pages: 560
ISBN-13:
DOWNLOAD EBOOKAuthor: Sook-Ying Ho
Publisher: Bentham Science Publishers
Published: 2010
Total Pages: 194
ISBN-13: 1608050246
DOWNLOAD EBOOKThis book deals with structural failure (induced by mechanical, aerodynamic, acoustic and aero-thermal, loads, etc.) of modern aerospace vehicles, in particular high-speed aircraft, solid propellant rocket systems and hypersonic flight vehicles, where structural integrity, failure prediction and service life assessment are particularly challenging, due to the increasingly more demanding mission requirements and the use of non-traditional materials, such as non-metallic composites, in their construction. Prediction of the complex loading environment seen in high-speed operation and constitutive / fracture models which can adequately describe the non-linear behaviour exhibited by advanced alloys and composite materials are critical in analyzing the non-linear structural response of modern aerospace vehicles and structures. The state-of-the-art of the different structural integrity assessment and prediction methodologies (including non-destructive structural health monitoring techniques) used for the structural design, service life assessment and failure analysis of the different types of aerospace vehicles are presented. The chapters are written by experts from aerospace / defence research organizations and academia in the fields of solid mechanics, and structural mechanics and dynamics of aircraft, rocket and hypersonic systems. The book will serve as a useful reference document containing specialist knowledge on appropriate prediction methodologies for a given circumstance and experimental data acquired from multi-national collaborative programs.