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1 - 10 of 19 search results for katalk:za31 24 / / / / / |u:www-civ.eng.cam.ac.uk where 0 match all words and 19 match some words.

  1. Results that match 1 of 2 words

  2. D:CURRENT_WORKMEMBRANE VIBRATION IN AIRSDM PAPERSDM_PAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1368.pdf
    18 Feb 2002: ma =ρ. k2s ω2airρ/B(24). If there is air on both sides of the membrane, the sameanalysis can be repeated to obtain an equation like(24), but with a factor ... 57.0 -4.24 84.4 70.2 67.1 -4.45 90.8 86.6 79.9 -7.7.

  3. K:PAPERSSPRINGBACK DESIGNPAPERSDM-PAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1498.pdf
    18 Feb 2002: 20 16 4.130 24 5.340 33 5.9. best-fit line through points 5-8 is 1 : 5. ... The long slits in the Configuration B dish, whichhas β = 24 deg, leave two long unsupportedlengths of skirt.

  4. 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.

  5. D:\Current_work\CRTS Reflectors\paper.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/CRTS_paper.pdf
    27 Aug 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.

  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. D:\Papers\Low-cost hinge report\report.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/report.pdf
    12 Jul 2002: 24. 4.4 Equation for ϑ1maxIn this case, the rotations vary approximately in a logarithmic manner. ... X. Z. tape measures. original positions. K zz. 1. Figure 5.24: Definition of extensional stiffness in z-direction.

  8. Space_Structures_Paper

    www-civ.eng.cam.ac.uk/dsl/publications/Space_Structures_Paper.pdf
    14 May 2002: γ tot2. .   .   γ tot π kα (24).

  9. D:\Current_work\Stiffened Springback ESTEC\paper.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/springback_paper.pdf
    27 Aug 2002: 20 16 4.130 24 5.340 33 5.9. 6. Table 3: Tested configurations. ... Configuration Cuts Slits α β γ w(deg) (deg) (deg) (mm). O - - - - - -A 2 2 - 4 50 20B - 4 8 24 90 20.

  10. Deployable Tensegrity Structures for Space Applications

    www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf
    30 Jul 2002: Calladine studies a physical model of a tensegritystructure with 12 joints and 24 bars, which should be loose with 6 degrees of freedom,according to Maxwell’s rule; yet, it is

  11. 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.

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