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  2. E:CURRENT_WORKCRTS TECHNOLOGYREPORT.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/TR195.pdf
    5 Apr 2001: Configuration 12 13.4. 24 3.6. Circular 6 45.9. Configuration 12 12.5. ... apertures of 1, 3, 5, and 10 m, with 6, 12, and 24 ribs.
  3. doi:10.1098/rspa.2005.1598

    www-civ.eng.cam.ac.uk/dsl/publications/Guest%20&%20Pellegrino.pdf
    2 Feb 2006: 24. 35 dq. dĈ. " #C/:. ð4:3ÞTo find equilibrium configurations of the structure, we look for points where. ... K̂ Zv2Û=vq2 v2Û=vq vĈ. v2Û=vq vĈ v2Û=vĈ2. 24. 35; ð4:5Þ. is positive definite.
  4. D:\Papers\Low-cost hinge report\report.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/report.pdf
    12 Jul 2002: 24. 4.4 Equation for ϑ1maxIn this case, the rotations vary approximately in a logarithmic manner. ... X. Z. tape measures. original positions. K zz. 1. Figure 5.24: Definition of extensional stiffness in z-direction.
  5. Computation of Buckling Pressure of Pumpkin Balloons

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2006-1803-983.pdf
    11 May 2006: n 16-48 64-96 112-145Elements along tendons 100 116 134Elements at equator 30 24 20Number of elements 3460 3216 3072Number of nodes 1831 1725 1671. ... Figures 24(a) and 24(b) show this type ofplot respectively for nCA118-10-290 and nCR118-10-290 balloons
  6. 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: cossin. ψψ. =. b (24). where ψ is the angular orientation of b and ranges π. ... Expanding Equation (23) with Equation (24) and writing the result in matrix form gives the stiffness in the ψ direction TKψ = b Kb (25) where.
  7. E:CURRENT_WORKDERA PROJECTSMALL SATELLITE MECHANISMSREPORT.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/TR190.pdf
    17 Nov 2000: 20. 3.4 Mass Estimates. 22. 3.5 Discussion. 22. 4 Deployable Reflector 24. ... 24. (Miura and Miyazaki 1990), in which the triangulated net was supported by six telescopic.
  8. Murphey et al AIAA-2003-1829 Traveler-ARM

    www-civ.eng.cam.ac.uk/dsl/publications/Murphey_AIAA_Traveler-ARM.pdf
    17 Feb 2003: α. α. =. =. (24). where I is the rotational inertia of a link. ... Again, the equation gives the average acceleration at time t. Equations (22) and (24) form a linear system of six equations with six unknowns.
  9. University of Cambridge Department of Engineering Vibration of…

    www-civ.eng.cam.ac.uk/dsl/publications/KukaMPhil.pdf
    25 Sep 2000: 4.8 Mode shapes of 10 m diameter re ector with 24 ribs. ... 24. 3.2. SIMPLE MEMBRANE STRUCTURE. Table 3.5: Natural frequencies of simple structure.
  10. C:\Documents and Settings\Sergio\My…

    www-civ.eng.cam.ac.uk/dsl/publications/Space-Frames_SDM_paper.pdf
    30 Mar 2004: W = PE δwsin2θcosθ. (23). But, since. φ =π. 2 2θ (24).
  11. Topology Optimization of Adaptive Compliant Aircraft Wing Leading…

    www-civ.eng.cam.ac.uk/dsl/publications/topology_paper_SDM.pdf
    2 Apr 2007: 24–33.3“SAMCEF v12.0-03,” Samtech Group, LIEGE science park, Rue des Chasseurs-Ardennais, 8B-4031 Liège (Angleur),.

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