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report1.dvi
www-civ.eng.cam.ac.uk/dsl/publications/TR170.pdf21 Mar 2001: TB =. 1. 24. 24b1 0 b2 0 b3 00 c1 0 c2 0 c3c1 b1 c2 b2 c3 b3. ... Figure 3.2: Equilibrium surface. 24. 0.2 0.1 0 0.1 0.2. 0.1. -
Computation of Buckling Pressure of Pumpkin Balloons
www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2006-1803-983.pdf11 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 -
D:\Papers\Low-cost hinge report\report.dvi
www-civ.eng.cam.ac.uk/dsl/publications/report.pdf12 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. -
Murphey and Pellegrino, NEM, AIAA-2004-1528, Rev 10
www-civ.eng.cam.ac.uk/dsl/publications/Actuated_tape_spring_SDM.pdf19 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. -
Murphey et al AIAA-2003-1829 Traveler-ARM
www-civ.eng.cam.ac.uk/dsl/publications/Murphey_AIAA_Traveler-ARM.pdf17 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. -
E:CURRENT_WORKDERA PROJECTSMALL SATELLITE MECHANISMSREPORT.DVI
www-civ.eng.cam.ac.uk/dsl/publications/TR190.pdf17 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. -
C:\Documents and Settings\Sergio\My…
www-civ.eng.cam.ac.uk/dsl/publications/Space-Frames_SDM_paper.pdf30 Mar 2004: W = PE δwsin2θcosθ. (23). But, since. φ =π. 2 2θ (24). -
University of Cambridge Department of Engineering Vibration of…
www-civ.eng.cam.ac.uk/dsl/publications/KukaMPhil.pdf25 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. -
SDM2003_1978.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Deployable_tensegrity_masts.pdf28 Feb 2003: Pak. Deployable tensegrity structures.Fourth-year undergraduate project report, 24 May2000. Department of Engineering, University ofCambridge, Cambridge, UK. -
Topology Optimization of Adaptive Compliant Aircraft Wing Leading…
www-civ.eng.cam.ac.uk/dsl/publications/topology_paper_SDM.pdf2 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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