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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. -
K:PAPERSSPRINGBACK DESIGNPAPERSDM-PAPER.DVI
www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1498.pdf18 Feb 2002: 20 16 4.130 24 5.340 33 5.9. best-fit line through points 5-8 is 1 : 5. ... The long slits in the Configuration B dish, whichhas β = 24 deg, leave two long unsupportedlengths of skirt. -
Space_Structures_Paper
www-civ.eng.cam.ac.uk/dsl/publications/Space_Structures_Paper.pdf14 May 2002: γ tot2. . . γ tot π kα (24). -
Implementation and Validation of Schapery-Rand Anisotropic…
www-civ.eng.cam.ac.uk/dsl/publications/paper.pdf18 May 2007: changes. Furtherinvestigation of this result is required. 2.98. 1.49. 0.00. 0.75. 2.24. -
D:\Papers\Rigid Deployable Array TR\report.dvi
www-civ.eng.cam.ac.uk/dsl/publications/TR214.pdf7 Jul 2004: 62 200 16.28 277. 90 273 24.8 177. - - 60.4 215. - - ... cannot be used to analyse this effect. 24. 3.2 Simulation with Pro/Mechanica. -
D:CURRENT_WORKEQUILIBRIUM_PATHSPAPER2.DVI
www-civ.eng.cam.ac.uk/dsl/publications/equilpath2.pdf16 Nov 1999: 24). Type 2 constraints prevent specified points Ci, at the corners of certain panels of wing 2,. ... 23. 7 Equilibrium path. 24. 8 Simulation of antenna deployment (connecting rods not shown). -
E:CURRENT_WORKKINEMATIC_BIFURCATIONS_IACMPAPER.DVI
www-civ.eng.cam.ac.uk/dsl/publications/kinematic.pdf28 Mar 2000: a2 b c = 0 (24). can be solved and, of the two solutions, the one closest ton1 is chosen. ... 24. 25. 26. 27. 28. 29. 30. 31. 32. 33. 3435. -
D:\Papers\Folding of composites\Paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Folding_of_composites_Paper.pdf6 May 2004: FOLDING OF WOVEN COMPOSITE STRUCTURES. J.C.H. Yee and S. Pellegrino1. Department of Engineering, University of CambridgeTrumpington Street, Cambridge CB2 1PZ, UK. ABSTRACT This paper investigates one-ply and two-ply laminates made from woven T300 -
D:\Papers\Optimization cover plates\cover-plates-paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/cover-plates-paper.pdf10 Jan 2004: US Patent,. 4,942,700. July 24, 1990. [5] Hoberman C. Radial expansion/retraction truss structures. ... mization. International Journal for Numerical Methods in Engineering 1987, 24:359–. 373. -
ABD Matrix of Single-Ply Triaxial Weave Fabric Composites A.B.H. ...
www-civ.eng.cam.ac.uk/dsl/publications/ABD%20matrix.pdf5 Apr 2007: lx ly (24). The outcome of this calculation is. . Nx. -
AIAA 2004-1529Multi-Configuration Space FramesT. Schioler and S.…
www-civ.eng.cam.ac.uk/dsl/Schioler/publications/SDM2004.pdf30 Jan 2005: W = PE δwsin2θcosθ. (23). But, since. φ =π. 2 2θ (24). -
report1.dvi
www-civ.eng.cam.ac.uk/dsl/publications/TR177.pdf21 Mar 2001: E. 266664. X1Y1::Z3. 377775 =. 24 aX bX cXaY bY cYaZ bZ cZ. ... 3.3. Prestressing Strategy 24. Tx1 = T1 tx1s1. Ty1 = ty1D1D2=2 (3.13). -
doi:10.1098/rspa.2005.1598
www-civ.eng.cam.ac.uk/dsl/publications/Guest%20&%20Pellegrino.pdf2 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.
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