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Titlebook: IUTAM-IASS Symposium on Deployable Structures: Theory and Applications; Proceedings of the I S. Pellegrino,S. D. Guest Conference proceedin

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書目名稱IUTAM-IASS Symposium on Deployable Structures: Theory and Applications
副標題Proceedings of the I
編輯S. Pellegrino,S. D. Guest
視頻videohttp://file.papertrans.cn/461/460657/460657.mp4
叢書名稱Solid Mechanics and Its Applications
圖書封面Titlebook: IUTAM-IASS Symposium on Deployable Structures: Theory and Applications; Proceedings of the I S. Pellegrino,S. D. Guest Conference proceedin
描述The IUTAM-IASS Symposium on Deployable Structures: Theory and Applications was held on 6-9 September 1998 in the Department of Engineering, University of Cambridge. The Scientific Committee was appointed jointly by the two sponsoring organisations, the International Union for Theoretical and Applied Mechanics (IUTAM) and the International Association for Shell and Spatial Structures (lASS). Its membership was as follows: S. Pellegrino (UK, Chairman) C. R. Calladine (UK) L. B. Freund (USA) M. Geradin (Belgium) Y. Hangai (Japan) K. Kawata (Japan) B. Kroplin (Germany) S. ]. Medwadowski (USA) M. M. Mikulas (USA) A. Samartin Quiroga (Spain) F. P. ]. Rimrott (Canada) T. Tarnai (Hungary) The opening lecture of the Symposium was given by Professor C. R. Calladine. It was followed by seven lecture sessions on Concepts, Structural Mechanics, Reflectors, Deployable Structures in Nature, Design and Testing, Inflatable Structures, Simulation, plus a large interactive session during which posters and physical models were shown. A discussion of topics suggested by the participants took place during the closing session. There were 83 participants from 18 countries, and a total of 50 papers were pr
出版日期Conference proceedings 2000
關鍵詞Fundament; Tensegrity; control; design; dynamics; finite element method; insects; mechanics; simulation; spac
版次1
doihttps://doi.org/10.1007/978-94-015-9514-8
isbn_softcover978-90-481-5539-2
isbn_ebook978-94-015-9514-8Series ISSN 0925-0042 Series E-ISSN 2214-7764
issn_series 0925-0042
copyrightSpringer Science+Business Media Dordrecht 2000
The information of publication is updating

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Inflatable Tensioned Membrane Waveguide Antenna Array for Space Applications,olving small spacecraft. Examples of these mission applications include microwave communications, synthetic aperture radar (SAR) and Earth Science remote sensing; as well as inter-planetary missions such as very long baseline interferometry. Many of these missions require the use of large aperture a
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Wing Folding in Beetles,on it is imperative that their delicate membranes can be safely stowed away when not in use. Dragonflies are one of the few groups to rest with the wings fully outstretched, the others having a basal hinge that allows the wings to be drawn automatically towards the body when they stop flying. Detail
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Symmetry as a Basis for Morphological Analysis and Generation of NASA-Type Cubic Deployables,analysis and modeling of several of NASA’s deployable truss structures by Alan Britt in 1997 in our Morphology Studio. In late 1997 we undertook to define a morphological method of generating deployable structures, based on crystallographic symmetry. Having modeled and developed variants for three N
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Design, Construction and Testing of the Deployable UHF Antenna for Skynet 4 Stage 2,ced version of the Stage 1 satellites with tuneable UHF, increased UHF transponder power, and new Earth-cover helical UHF antenna designed and built by AEA Technology. The contract for the supply of the flight UHF antennas was awarded following the successful testing of the Qualification Model anten
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Foldable Rigid Connections,owever, for terrestrial structures subjected to the gravity load, wind load or inertia force due to earthquakes, moment frames consisting of beams, columns and connections with bending moment rigidity are often constructed. In the paper a key idea is proposed to make such moment frames foldable. A s
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