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51 - 60 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. AIAA 2004-1529Multi-Configuration Space FramesT. Schioler and S.…

    www-civ.eng.cam.ac.uk/dsl/Schioler/publications/SDM2004.pdf
    30 Jan 2005: Figure 20 shows the measured force-displacement characteristics as well as the theoreticalresponse derived by assuming elastic axial shorteningand Euler buckling. ... 10. 15. Force. (N). Displacement (mm). Fig. 20 Comparison of theoretical and

  3. NEW CONCEPTS FOR SPACECRAFT ANTENNAS AND RADAR STRUCTURESBASED ON ...

    www-civ.eng.cam.ac.uk/dsl/publications/New%20concepts.pdf
    17 Feb 2006: 10. 0.0. 0.5. 1.0. 1.5. 2.0. 0 5 10 15 20.

  4. A Numerical Approach to the Kinematic Analysis of Deployable ...

    www-civ.eng.cam.ac.uk/dsl/publications/Numerical_approach.pdf
    20 Mar 2006: This transformed equation can be treated in the same way as Equation 20, thus rearranging it. ... Guest. 31. 0 20 40 60 80 100 1200. 1.0. 2.0.

  5. D:\Papers\Rigid Deployable Array TR\report.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/TR214.pdf
    7 Jul 2004: with the offset. 0 10 20 30 40 50 60 70 80 900. ... deployment moments for negative rotations. 0 20 40 60 80 100 120 140 160 180 2001.

  6. SDM2003_1978.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Deployable_tensegrity_masts.pdf
    28 Feb 2003: 2American Institute of Aeronautics and Astronautics. -10 -5 0 5 10 15 20 25 30. ... International Journal of Solids and Structures,30(21):3025–3035, 1993. [20] A. Micheletti. On the kinematics of tenseg-rity towers.

  7. E:CURRENT_WORKKINEMATIC_BIFURCATIONS_IACMPAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/kinematic.pdf
    28 Mar 2000: n (20)then the root has already been found and the next starting point is considered. ... 13. 14. 15. 16 17. 18. 19. 20. 21. 22. 23.

  8. Design & Manufacture of Stiffened Spring-Back Reflector…

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2005-2048.pdf
    17 May 2005: Hence the curvedstiffener is a circular arc of r = 20 mm subtending anangle of 69. ... The first 20 eigenmodes wereextracted and the maximum frequency of interest wasset to 40 Hz.

  9. D:CURRENT_WORKWRINKLES COMPUTATIONSDM_2002_PAPERSDM-PAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1369.pdf
    22 Mar 2002: web”. Zeitschrift für Flugtechnik Motorlurftschiffahrt, Vol. 20,1929. 2Reissner, E., “On tension field theory”, Proc. ... 20, pp. 631–639, 1985. 14Adler, A.L., Mikulas, M.M., and Hedgepeth, J.M., “Staticand dynamic analysis of partially

  10. Modelling of Anisotropic Viscoelastic Behaviour in Super-Pressure…

    www-civ.eng.cam.ac.uk/dsl/publications/Anisotropic%20viscoelastic%20behaviour.pdf
    10 Apr 2007: 40 -20 0 2002468. 10. Temperature [oC]. Log a. T. 0 4 8 12 16 20 24. ... 3. 4. time [s]. str. ess [M. Pa]. 0 20 40 60 5200.

  11. Wrinkled membranesPart I: experiments

    www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p02-p.pdf
    23 Feb 2006: 0 0.5 1 1.5 2 2.5 310. 15. 20. 25. 30. ... membrane, because the corner attachments could only carry a maximum load ofonly 20 N.

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