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IStructE 2003 Poster
www-civ.eng.cam.ac.uk/dsl/ppao2/documents/IStructE_2003_Poster.pdf22 May 2003: 4 8 12 16 20 24 28 32 36 401.0. 1.1. -
C:\Documents and Settings\Sergio\My Documents\Papers\Wrinkled…
www-civ.eng.cam.ac.uk/dsl/publications/Barcelonapaper.pdf24 Apr 2003: λ(δ1 δ2)π. (24). Here δ1 and δ2 are the radial displacements of the corners loaded by T1 and T2, respectively;these corner displacements can be estimated from. ... The wavelength predictions are very close.The wrinkle amplitudes have been estimated -
D:\Current_work\Closed-Loop Linkages\SDM_paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Closed-loops_SDM.pdf14 Feb 2003: weobtain. T1TĀT3TB̄T1TC̄T3TD̄. (T1UĀT3TB̄T1TC̄T3TD̄) θ′A+(T1TĀT3UB̄T1TC̄T3TD̄) θ′B+(T1TĀT3TB̄T1UC̄T3TD̄) θ′C+(T1TĀT3TB̄T1TC̄T3UD̄) θ′D = I (24). From Equation 23, the first term in Equation 24 isequal to I E. -
March 12, 2003 11:8 Proceedings of OMAE’0322nd International…
www-civ.eng.cam.ac.uk/dsl/publications/OMAE2003-37465.pdf14 Mar 2003: e11 =h1A2 h2A1. (h1h3 h22)|V |(23). e12 =h3A1 h2A2. (h1h3 h22)|H|(24). ... At this. 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 401. -
April 30, 2003 18:33 Proceedings of OMAE’0322nd International…
www-civ.eng.cam.ac.uk/dsl/ppao2/documents/OMAE2003-37465.pdf22 May 2003: e11 =h1A2 h2A1. (h1h3 h22)|V |(23). e12 =h3A1 h2A2. (h1h3 h22)|H|(24). ... At this. 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 401. -
D:\Papers\Foldable composite structures-IASS\Paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/FoldableCompStruc.pdf15 Aug 2003: Yee, J.C.H. and Pellegrino, S. (2003b) Folding of composite structures. Conference onDeformation and Fracture of Composites (FRC-7), Sheffield University, 22-24 April2003. -
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. -
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.pdf14 Feb 2003: θm = νσrE. (24). Wrinkles will form when the geometric hoop strainis larger than the material strain, hence from Equa-tions 8, 22, 23 and 24, we obtain. ... t (mm) Eq. 37 (mm) Exp. (mm) FE (mm). 0.025 24.7 25.4 22.30.050 41.5 33.9 35.6. -
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. -
Murphey and Hinkle, Hierarchical Space Structures AIAA 200–
www-civ.eng.cam.ac.uk/dsl/publications/HierarchicalSpaceStructures.pdf23 Apr 2003: π= (24). The battens and diagonals must provide enough support to the longerons to enforce local buckling.
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