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31 - 40 of 73 search results for :pc53 24 / |u:www-civ.eng.cam.ac.uk where 0 match all words and 73 match some words.

  1. Results that match 1 of 2 words

  2. SDM2003_1978.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Deployable_tensegrity_masts.pdf
    28 Feb 2003: Pak. Deployable tensegrity structures.Fourth-year undergraduate project report, 24 May2000. Department of Engineering, University ofCambridge, Cambridge, UK.

  3. Murphey and Hinkle, Hierarchical Space Structures AIAA 200–

    www-civ.eng.cam.ac.uk/dsl/publications/HierarchicalSpaceStructures.pdf
    23 Apr 2003: π= (24). The battens and diagonals must provide enough support to the longerons to enforce local buckling.

  4. Thin-Shell Deployable Reflectors with Collapsible Stiffeners: Part I…

    www-civ.eng.cam.ac.uk/dsl/publications/Reflectors-with-stiffeners.pdf
    1 Mar 2005: C90 2.72 24.76 4.18 39.18 0.274. Table 3. Comparison of optimized Configuration D. ... 24 of 28. Tan & Pellegrino. of given width and thickness, shortening the slits at the end of diameter d1 increases the.

  5. SDM04.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Ultrathin_antennas_Paper.pdf
    31 Mar 2004: Resulting in λ = 7.11 104and a corresponding fundamental natural frequency of0.24 Hz.†.

  6. 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.

  7. 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.pdf
    14 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.

  8. D:\Papers\Bistable prestressed shells\Paper.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Kebadze-Guest-Pellegrino_revised.pdf
    17 Feb 2004: 4Test. -4-21 23 -24. Analysis -26 24 -26. 5Test. -3.2-18 36 -22. ... shell; the configurations (b-d) are unstable. 24. Figure 3: Sliced-up shell.

  9. D:\Papers\Amplitude_of_wrinkles\paper.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/amplitude_of_wrinkles.pdf
    3 Jun 2002: Ub =Et3. 24(1 ν2). (12Hλ. 2H0. λ0. κ2ηdξdη. )=. Et3. 24(1 ν2)π4A2. ... U =(1 ν)Etγ. 2. (π2t2. 24(1 ν2)λ2 γλ2. 8H2. )(23). which is minimised by differentiating with respect to λ.

  10. Viscoelastic Behaviour of Pumpkin Balloons T. Gerngross, Y. Xu ...

    www-civ.eng.cam.ac.uk/dsl/publications/viscoelastic%20behaviour%20of%20pumpkin%20balloons.pdf
    17 Apr 2007: 0 4 8 12 16 20 24. -1.2. -0.8. -0.4. 0.0.

  11. Wrinkled membranesPart II: analytical models

    www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p03-p.pdf
    23 Feb 2006: 12(1 ν2)π 4 A2. 4λ4. (24). The stretching strain energy per unit area can be obtained, neglecting stretchingin the η-direction, from. ... U =(1 ν)E t γ. 2. (π 2t 2. 24(1 ν2)λ2+.

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