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21 - 30 of 83 search results for TALK:PC53 20 |u:www-civ.eng.cam.ac.uk where 0 match all words and 83 match some words.

  1. Results that match 1 of 2 words

  2. E:CURRENT_WORKCRTS DEMONSTRATORREPORT.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/CRTS2001.pdf
    21 Mar 2001: Rits. ESTEC Contract no. 11936/96/NL/FG. Release date: 20 March 2001. Abstract. ... 17. 18. 19. 20. 21. 22. 23. 24. Rm [mm]. Rr[mm] Rr = 0.4957Rm 6.7181.

  3. E:CURRENT_WORKBI-STABLE_SHELLS_SDMPAPER_SDM.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/bistable.pdf
    8 Feb 2000: 0 5 10 15 20 25 30 35 400. 0.1. 0.2. ... 7American Institute for Aeronautics and Astronautics. 0 5 10 15 20 25 30 35 40.

  4. University of Cambridge Department of Engineering Vibration of…

    www-civ.eng.cam.ac.uk/dsl/publications/KukaMPhil.pdf
    25 Sep 2000: 18. 3.1.3 FE Analysis using Truss Elements. 20. 3.1.4 Results. 22. ... Parameter Rib Membrane. Density (kg/m3) 7000 1. Young's Modulus (GPa) 200 20.

  5. Thermo-Elastic Behaviour of Single Ply Triaxial Woven Fabric…

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2006-1899-892.pdf
    11 May 2006: 20 30 40 50 60 70 80 90 100 110 120-1.5. ... There are 20 hexagon units and 10 unit cells in these strips, respectively.

  6. D:CURRENT_WORKTSR HINGEPAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/TSR_hinge.pdf
    21 Jan 2002: 0.07 -0.06 -0.05 -0.04 -0.03 -0.02 -0.01 0 0.01-24. -20. ... 0.05 -0.04 -0.03 -0.02 -0.01 0-20. -18. -16. -14. -12.

  7. Deployable Tensegrity Structures for Space Applications

    www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf
    30 Jul 2002: 42. Abbreviations. ACeS Asia Cellular Satellite, p. 20. ADAM Able Deployable Articulated Mast, p. ... 18. LaRC NASA Langley Research Center, p. 20. LDR Large Deployable Reflector, p.

  8. Tape Spring Large Deployable Antenna

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2006-1601-386.pdf
    11 May 2006: 20. -15. -10. 0 40 80 120 160. Abov e -ground biomass (tons/ha). ... Thus, the structure consists of two curved cylindrical face-sheets 20 mm apart, with internal unidirectionalribbing, strengthening the longitudinal direction of the antenna.

  9. E:/Diplomarbeit/Latex/Thesis.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Schultheiss_Diploma_paper.pdf
    12 Nov 2003: 20. 3.11 The Trolley and the Rail. 22. 3.12 Graphical Description of the Basic Restrictions. ... 36. 3.19 Detailed View of Hinge Line H1. 37. vi. 3.20 Experimental Method to Determine the Moment in the Hinge Line: Measuring theDeflection of the Plumb-Bob

  10. Micromechanical Models for Bending Behavior of Woven Composites

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2005-2264.pdf
    17 May 2005: 0. 100. 200. 300. 400. 500. 600. 0.00 0.20 0.40 0.60 0.80 1.00 1.20. ... 15. 20. 25. 0.00 0.03 0.06 0.09 0.12. Curvature (1/mm). Mo.

  11. E:CURRENT_WORKSPRING-BACK REFLECTORPAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/springback.pdf
    27 Mar 2000: 8. IASS-IACM 2000, Chania – Crete, Greece. 20 30 40 50 60 70 80 90. ... The segments of the skirt to which loadsare applied snap atP 20 N and the deformation of the reflector can be seen in Figure 8.

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