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41 - 50 of 231 search results for KaKaoTalk:ZA31 24 24 |u:www-civ.eng.cam.ac.uk where 0 match all words and 231 match some words.

  1. Results that match 1 of 2 words

  2. LATERAL SPREADING OF SLOPES

    www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR317.pdf
    28 Feb 2002: Figure 23: Pore pressures measured in test SKH-11 35 Figure 24: Accelerations measured in test SKH-12 37. ... of approximately 20% magnitude. No significant ground displacement was measured. The results of test SKH-12 are plotted in Figure 24.

  3. LATERAL SPREADING OF SLOPES

    www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR318.pdf
    4 Mar 2002: 4.5 Test SKH-17 The results of test SKH-17 are plotted in Figures 21-24. ... PPT2259. PPT6669. PPT6794. PPT6260. Max= 7.18. Min= 4.92. Max= 64.1. Min= 24.2.

  4. E:CURRENT_WORKDERA PROJECTSMALL SATELLITE MECHANISMSREPORT.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/TR190.pdf
    17 Nov 2000: 20. 3.4 Mass Estimates. 22. 3.5 Discussion. 22. 4 Deployable Reflector 24. ... 24. (Miura and Miyazaki 1990), in which the triangulated net was supported by six telescopic.

  5. with a viewfor use ast are beingns. A widethat ...

    www-civ.eng.cam.ac.uk/cjb/papers/p51.pdf
    25 Apr 2005: with a viewfor use ast are beingns. A widethat are notdels. Thet also that. tressing. Statistical Lifetime Predictions for Aramid FibersK. G. N. C. Alwis1 and C. J. Burgoyne2. Abstract: This paper investigates the statistical procedures that can be

  6. C:\Documents and Settings\Administrator\My…

    www-civ.eng.cam.ac.uk/dsl/publications/Reflector2002.pdf
    14 May 2002: Offset 6 45.9Configuration 12 12.5(A = 1 m) 24 3.3. Table 1: Typical surface errors of reflectors with D =10 m and F = 7.8 m.

  7. Fracture Mechanics of Plate DebondingP. M. M. Achintha1 and ...

    www-civ.eng.cam.ac.uk/cjb/papers/p59.pdf
    22 Mar 2010: Fracture Mechanics of Plate DebondingP. M. M. Achintha1 and C. J. Burgoyne2. Abstract: This paper presents a fracture mechanics model to determine the load at which FRP plates will debond from reinforcedconcrete beams. This will obviate the need for

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

    www-civ.eng.cam.ac.uk/dsl/publications/New%20concepts.pdf
    17 Feb 2006: A T300/LTM45 plain weave CFRP, 3-ply laminate (0/45/0) with uniform thickness wasadopted.Rmin was set at 24 mm, which provides a margin of 2.3 on material

  9. Osman, A. S., Mair, R. J. & Bolton, M. ...

    www-civ.eng.cam.ac.uk/geotech_new/people/bolton/mdb_pub/176.pdf
    16 Nov 2006: 2.89 3.13 1.76 1.99 0.62 0.841 4.46 4.76 3.35 3.64 2.24 2.51 1.11 1.37. ... 2.72 22.450.5 9.62 9.72 6.39 6.53 3.15 3.34 0.11 0.140.75 12.10 12.24 8.88 9.06

  10. D:\Papers\Foldable composite structures-IASS\Paper.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/FoldableCompStruc.pdf
    15 Aug 2003: Yee, J.C.H. and Pellegrino, S. (2003b) Folding of composite structures. Conference onDeformation and Fracture of Composites (FRC-7), Sheffield University, 22-24 April2003.

  11. SEISMIC MODELLING OF EMBANKMENTSON SAmRATED SOIL DEPOSITS.…

    www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR300.pdf
    17 Aug 2001: 1 5 01. ACCs 7 max=24.59. 1258 $j min=-27.760 0.05 0.1 0.15 02.

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