Scaling Effects in the Static and Dynamic Response of Graphite-epoxy Beam-columns
Author | : Karen E. Jackson |
Publisher | : |
Total Pages | : 284 |
Release | : 1990 |
Genre | : Structural analysis (Engineering) |
ISBN | : |
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Author | : Karen E. Jackson |
Publisher | : |
Total Pages | : 284 |
Release | : 1990 |
Genre | : Structural analysis (Engineering) |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 602 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : American Society for Composites. Technical Conference |
Publisher | : CRC Press |
Total Pages | : 1168 |
Release | : 1993-10-15 |
Genre | : Technology & Engineering |
ISBN | : 9781566761031 |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 418 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Author | : D. Durban |
Publisher | : Springer Science & Business Media |
Total Pages | : 376 |
Release | : 2006-04-11 |
Genre | : Technology & Engineering |
ISBN | : 0306469545 |
The optimal control of flexible structures is an active area of research. The main body of work in this area is concerned with the control of time-dependent displacements and stresses, and assumes linear elastic conditions, namely linear elastic material behavior and small defor- tion. See, e. g. , [1]–[3], the collections of papers [4, 5], and references therein. On the other hand, in the present paper we consider the static optimal control of a structure made of a nonlinear elastic material and und- going large deformation. An important application is the suppression of static or quasi-static elastic deformation in flexible space structures such as parts of satellites by the use of control loads [6]. Solar rad- tion and radiation from other sources induce a temperature field in the structure, which in turn generates an elastic displacement field. The displacements must usually satisfy certain limitations dictated by the allowed working conditions of various orientation-sensitive instruments and antennas in the space vehicle. For example, a parabolic reflector may cease to be effective when undergoing large deflection. The elastic deformation can be reduced by use of control loads, which may be imp- mented via mechanically-based actuators or more modern piezoelectric devices. When the structure under consideration is made of a rubb- like material and is undergoing large deformation, nonlinear material and geometric effects must be taken into account in the analysis.
Author | : J M Hodgkinson |
Publisher | : Elsevier |
Total Pages | : 379 |
Release | : 2000-10-27 |
Genre | : Technology & Engineering |
ISBN | : 1855738910 |
Testing of composite materials can present complex problems but is essential in order to ensure the reliable, safe and cost-effective performance of any engineering structure. This essentially practical book, complied from the contributions of leading professionals in the field, describes a wide range of test methods which can be applied to various types of advanced fibre composites. The book focuses on high modulus, high strength fibre/plastic composites and also covers highly anisotrpoic materials such as carbon, aramid and glass.Engineers and designers specifying the use of materials in structures will find this book an invaluable guide to best practice throughout the range of industrial sectors where FRCs are employed.
Author | : Josef Singer |
Publisher | : John Wiley & Sons |
Total Pages | : 644 |
Release | : 1998-02-11 |
Genre | : Technology & Engineering |
ISBN | : 9780471956617 |
Written by eminent researchers and renown authors of numerous publications in the buckling structures field. Deals with experimental investigation in the industry. Covers the conventional and more unconventional methods for testing for a wide variety of structures. Various parameters which may influence the test results are systemically highlighted including, imperfections, boundary conditions, loading conditions as well as the effects of holes and cut-outs.