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1 - 10 of 11 search results for TALK:PC53 20 |u:www-civ.eng.cam.ac.uk where 0 match all words and 11 match some words.

  1. Results that match 1 of 2 words

  2. CUED Bridge Research - Publications

    www-civ.eng.cam.ac.uk/brg/papers/
    29 Sep 2004: Imhof,D. Probabilistic Safety Assessment of Existing Bridges. The Young Researchers' Conference, 20 March 2002, Poster Presentation: The Institution of Structural Engineers, Upper Belgrave Street, London.

  3. D:\Papers\Folding of composites\Paper.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Folding_of_composites_Paper.pdf
    6 May 2004: European Journal of Mechanics A/Solids, 2001;20:23-37. 6. Table 1: Properties of fibres and resinsT300 913 914. ... 10. 20. 30. 40. 50. 60. 70. 80. Figure 5: Stress-strain response from in-plane shear test on one-ply T300/913.

  4. C:\Documents and Settings\Sergio\My Documents\Current_work\CFRP tape…

    www-civ.eng.cam.ac.uk/dsl/publications/CFRP_tape_springs_Paper.pdf
    9 Apr 2004: 20 to 22 into Eq. 23, and minimiz-ing the total bending energy with respect to r yields. ... 24 and 20 into Eq. 21, and multi-plying by the arc length of the tape, Rθ.

  5. D:\Papers\Optimization cover plates\cover-plates-paper.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/cover-plates-paper.pdf
    10 Jan 2004: each side, hence N = 20 design variables in total, and the hinge size is not considered. ... 20. Figure 19: Optimized plate shape when all three weight factors are equal to one.

  6. 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.

  7. C:\Documents and Settings\Sergio\My…

    www-civ.eng.cam.ac.uk/dsl/publications/Space-Frames_SDM_paper.pdf
    30 Mar 2004: Figure 20 shows the measured force-displacement characteristics as well as the theoreticalresponse derived by assuming elastic axial shorteningand Euler buckling. ... 15. Force(N). Displacement (mm). Fig. 20 Comparison of theoretical and experimen-tal

  8. SDM04.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Ultrathin_antennas_Paper.pdf
    31 Mar 2004: 1. 2. 3. 1.676 CFRP. 0.3048 CFRP. 0.6 epoxy 10.7 epoxy 20.8 CFRP. ... b) Side elevation. Fig. 11 Distortion of reflector without stiffener (magnified by 20).

  9. Murphey and Pellegrino, NEM, AIAA-2004-1528, Rev 10

    www-civ.eng.cam.ac.uk/dsl/publications/Actuated_tape_spring_SDM.pdf
    19 Apr 2004: D Q. (20). Equilibrium and Stability Analysis. According to the principle of minimum potential energy, equilibrium configurations exist when the instantaneous rate of change of strain energy density with respect to ... 75. -25. -50. -75. 20-20 40-40 60-60

  10. D:\Current_work\Asymmetrically-Bistable Structure…

    www-civ.eng.cam.ac.uk/dsl/publications/Asymmetrically-Bistable_SDM_Paper.pdf
    29 Mar 2004: 0 5 10 15 20 25 30 35. 0.1. 0.2. 0.3. ... s =v2. 2g(16). 5. 10. 15. 20. 25. 0.5. 1. 1.5.

  11. D:\Current_work\Deployable_Reflector_Concept_SDM\Paper_SDM.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Reflector_concept_Paper.pdf
    29 Mar 2004: 0.0. 0.5. 1.0. 1.5. 2.0. 0 5 10 15 20. Displacement (mm). ... 20 Packaged demonstrator. 10 of 11. American Institute of Aeronautics and Astronautics Paper 2004-1574.

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