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15 May 2003: failure) (MPa) 17.83 4.3 18.78 qb/qc (D/10 failure) 0.60 0.53 0.63 Qb (plunging failure) (kN) 830 200 640 Pile head load continues to ... 0. 100. 200. 300. 400. 500. 600. 0 10 20 30 40.

13 Oct 2003: the model at 200g. 0. 129. 200221. 0. 50100150. 200250. 0 100 200 300 400Radial distance (mm).

22 Jun 2003: tens of millimetres. A survey of approximately 200 concrete highway bridges in the. ... 1.0. 2.0. 3.0. 4.0. 5.0. 6.0. 7.0. 8.0. 9.0. 10.0. 0.0 50.0 100.0 150.0 200.0

15 Oct 2003: 2(d). Measurements have been conducted on three samples of average mass 200 g each. ... 25. (b). 200 µm. (a). 200 µm. (c) (d). 100 200 300 400 500 600 700 8000.

3 Mar 2003: 0 50 100 150 200 250 300 350-2. -1.5. -1. -0.5.

22 May 2003: 0 100 200 300 400 500 600 700 800. LOAD (kN).

14 Feb 2003: 0 200 400 600Distance, η (mm). Experiment ABAQUS. -1. 0. 1. ... 1. 0. 1. 2. Experiment ABAQUS. w (. mm. ). 0 50 100 150 200.

12 Nov 2003: Universität Stuttgart University of Cambridge. Institut für Department of EngineeringStatik und Dynamik. Gravity Compensation of Deployable Solar Arrays. for Small Spacecraft. Diploma Thesis submitted to the Universität Stuttgart. for the

23 Apr 2003: 200 04w dπρ= (5). where E is Young’s modulus and ρ is the bulk material weight density. ... 0.1. 0.01. 1. 10. Ele. men. t Dia. met. er (. mm. ) E = 200 GPaL = 10 mP = 100 N.

15 Aug 2003: 4. involved 200 elements lengthwise by 30 elements widthwise. The mesh for a completetape tube hinge had a similar mesh density and hence the number of elements wasproportionally larger.