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D:\Papers\Vibration wrinkled membranes SDM\SDM_Paper_2003.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Vibration_wrinkled_membranes_SDM.pdf14 Feb 2003: Mode 22 (41.81 Hz) Mode 23 (41.98 Hz) Mode 24 (44.32 Hz). -
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. -
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. -
1 Author’s contact details: R. J. Lock, Graduate Engineer, ...
www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR320.pdf22 Jun 2003: 24 4.4 Field Study of an Integral Backwall Bridge: Hoppe & Gomez, 1996. ... 24. ntegral backwall bridge. he others presented in this report in that it is an integral. -
p1aper1003.dvi
www-civ.eng.cam.ac.uk/geotech_new/people/bolton/mdb_pub/144_Acta_2004_52_(12)_3587-3601.pdf15 Oct 2003: river sand (CU = 2.24) and Berlin sand (CU = 2.27) [11]. ... 33. 24. pressure. transducer. to vacuum pump. reflective. laser. device. emission/reception. -
E:/Diplomarbeit/Latex/Thesis.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Schultheiss_Diploma_paper.pdf12 Nov 2003: 24. 3.13 Example of two Non-holonomic Restrictions Being Violated and its Handling. ... Time. 41. 3.24 Force of Static Friction vs. Normal Force. 41. -
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. -
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. -
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. -
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.
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