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Numerical modelling of theelectrokinetic remediation ofheavy metal…
www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR292.pdf17 Aug 2001: a; = wiai (7). u; = op; (8). and 0,: = w,D, (9). -
University of Cambridge Department of Engineering Vibration of…
www-civ.eng.cam.ac.uk/dsl/publications/KukaMPhil.pdf25 Sep 2000: Then, in the next step(frequency extraction step), the boundary conditions are changed to the actualones, described above, by using BOUNDARY, OP=NEW option. -
Thin-Shell Deployable Reflectors with Collapsible Stiffeners: Part I…
www-civ.eng.cam.ac.uk/dsl/publications/Reflectors-with-stiffeners.pdf1 Mar 2005: Figure 14 compares the load-displacement relationship of this optimised structure (Op-. -
Wrinkled membranesPart II: analytical models
www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p03-p.pdf23 Feb 2006: R2 = R1(. sinπ. 4 θ1. )/(sin. π. 4 θ2. ). (50). For the second condition, apply the sine rule to D′OP to obtain. -
E:CURRENT_WORKDERA PROJECTSMALL SATELLITE MECHANISMSREPORT.DVI
www-civ.eng.cam.ac.uk/dsl/publications/TR190.pdf17 Nov 2000: Small Satellite Deployment. Mechanisms. S. Pellegrino, S. Kukathasan, G. Tibert. and A. Watt. CUED/D-STRUCT/TR190. The work presented in this report was partially supported by research contract no. CU009-. 0000004842 between the Defence Evaluation -
Deployable Tensegrity Structures for Space Applications
www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf30 Jul 2002: TRITA-MEK Technical Report 2002:04 ISSN 0348-467XISRN KTH/MEK/TR--02/04--SE. Deployable Tensegrity Structuresfor Space Applications. Gunnar Tibert. Royal Institute of TechnologyDepartment of Mechanics. Doctoral ThesisStockholm, 2002. Deployable
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