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  2. Chris Morley

    www-civ.eng.cam.ac.uk/struct/ctm/publications.html
    30 Nov 2007: 1986 - 1990 L.B.B.Peer Ph.D. thesis 1990 Water flow into unsaturated concrete. ... ACI Structural Journal, 87, 597-605. 1991 (Z.B.Mohamed & CTM) Shear strength of r.c.
  3. D:\Current_work\Deployable_Reflector_Concept_SDM\Paper_SDM.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Reflector_concept_Paper.pdf
    29 Mar 2004: A. B. B. A. (a) Flat. (b) Deployed. Fig. 2 Use of a shaped sheet A to form sheet Binto a singly-curved surface. ... Surface A. O. y. D, G. L. M. C. E. (b) Folded configuration.
  4. C:\Documents and Settings\Sergio\My Documents\Papers\Wrinkled…

    www-civ.eng.cam.ac.uk/dsl/publications/Barcelonapaper.pdf
    24 Apr 2003: w. R. r1. π/2n. Rwrin-r1. θ. r. (a). (b). λ. 2A. ... A. B. B. C. C. (b). Figure 5: Wrinkled shapes for (a) T1/T2 = 1 and (b) T1/T2 = 4.
  5. NEW CONCEPTS FOR SPACECRAFT ANTENNAS AND RADAR STRUCTURESBASED ON ...

    www-civ.eng.cam.ac.uk/dsl/publications/New%20concepts.pdf
    17 Feb 2006: A. B. B. A. (a) Flat. (b) Deployed. Figure 2: Use of a shaped sheet A to shape sheet B into a singly-curved surface. ... The required reflective surface is obtained by replacing sheet B with a rectangular sheet, see.
  6. Micromechanical Models for Bending Behavior of Woven Composites

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2005-2264.pdf
    17 May 2005: . N. M.  =. . A. B. B. D. . ... It is assumed that the laminate is symmetric B = 0,and is subject to pure bending and large curvature κx,i.e.
  7. IASS-IACM 2000Fourth International Colloquium on Computation of Shell …

    www-civ.eng.cam.ac.uk/dsl/publications/slittube.pdf
    13 Sep 2000: them. (a) Extended configuration (b) Coiled configuration. Figure 1:The two equilibrium states. ... b) Symmetrical layup. Figure 11:Contours ofΓXY for the two layups. for zero global force.
  8. D:\Current_work\Wrinkles in solar sails SDM\SDM_2003\SDM-paper-03.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Wrinkle-amplitudes-solar-sails_SDM.pdf
    14 Feb 2003: An. A. A. B. B. C. C. η. ξw. Fig. 12 Wrinkle details for T1/T2 = 4. ... a) (b). (c) (d). Fig. 13 Shapes of membrane for T1/T2 equal to (a)1, (b) 2, (c) 3, (d) 4.
  9. Murphey and Pellegrino, NEM, AIAA-2004-1528, Rev 10

    www-civ.eng.cam.ac.uk/dsl/publications/Actuated_tape_spring_SDM.pdf
    19 Apr 2004: σ. (11). The A and B stiffness matrices of CLT and are given by. ( ). ( ). ... grad gradK D D u uψ = = b b b b (23) where b is the unit vector in the direction of the derivative.
  10. E:CURRENT_WORKDERA PROJECTSMALL SATELLITE MECHANISMSREPORT.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/TR190.pdf
    17 Nov 2000: a). (b). (d). (c). Additionalmembers. Figure 4.2: New concept. 27. (a) (b). ... Figure 4.3: Hexagonal tensegrity module; (a) three-dimensional view; (b) top view.
  11. A Numerical Approach to the Kinematic Analysis of Deployable ...

    www-civ.eng.cam.ac.uk/dsl/publications/Numerical_approach.pdf
    20 Mar 2006: shown) and (b) deployed. 22. 6 Elementary transformations between coordinate systems for a rod. ... A B. (b)(a). zC. CZ. zA. O. A. v1. rod 1.
  12. C:\Documents and Settings\Sergio\My Documents\Current_work\CFRP tape…

    www-civ.eng.cam.ac.uk/dsl/publications/CFRP_tape_springs_Paper.pdf
    9 Apr 2004: 1(b), in which case the edges of the tapespring are subject to tensile stresses. ... . N.M.  =. . A. B. B. D. . .
  13. Topology Optimization of Adaptive Compliant Aircraft Wing Leading…

    www-civ.eng.cam.ac.uk/dsl/publications/topology_paper_SDM.pdf
    2 Apr 2007: 7 8 9. (b). 5 6 7. 9 10 11. 13 14 15. ... 13. 16. 1514. A. B. (b) Parent lattice realisation. Figure 7.
  14. Wrinkled membranesPart III: numerical simulations

    www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p04-p.pdf
    23 Feb 2006: 0.5. 0. 0.5. 0 100 200 300 400. (a) (b). (c) (d). ... B. B. C. C. O. Figure 15. Wrinkled shape for T1 = 20 N and T2 = 5 N (amplified10 times).
  15. report1.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/TR177.pdf
    21 Mar 2001: 12. 2.6 Projections of circular conguration onto (a) global plane; (b) localplane. ... β. (b). B. R. D. C. D. B CO. (a). 2 R.
  16. Deployable Tensegrity Structures for Space Applications

    www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf
    30 Jul 2002: 35. W Right singular matrix (b b), p. 55X, Y, Z Coordinates in global system (parent paraboloid), p. ... Φ Matrix of bar flexibilities (b b), p. 59ω Element stress (equivalent to q), p.

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