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41 - 50 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. E:CURRENT_WORKTENSEGRITY REFLECTORSDM_PAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/AGT-SP_paper.pdf
    6 Feb 2001: 6American Institute for Aeronautics and Astronautics. 0 5 10 15 20 25 300. ... 20. r =δ2 R2 sin2 (θ/2). 2δ(19). γ = 2 arccosr δ.

  3. C:DOCUMENTS AND SETTINGSADMINISTRATORMY…

    www-civ.eng.cam.ac.uk/dsl/publications/tensereflect.pdf
    10 Nov 2001: nodes. 19. Figure 8: Loads applied to cable net. 20. 1.631.13. ... 23. 0 5 10 15 20 25 30-0.5. 0. 0.5. 1.

  4. 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.

  5. D:CURRENT_WORKMEMBRANE VIBRATION IN AIRSDM PAPERSDM_PAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1368.pdf
    18 Feb 2002: ks = 2π. 1. λ2sx+. 1λ2sy. (20). and the corresponding natural frequency of vibrationin vacuum from Equation (6). ... apply-ing bi-axial uniform prestress of 20 N/m to allmembrane elements. •

  6. report_final.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/TR192.pdf
    21 Mar 2001: 20. 4 Results 22. 4.1 Introduction. 224.2 Phase II Results. 224.3 Phase III Results. ... 250. 300. (a) 8 ribs. 0 10 20 30 40 50 60 700.

  7. 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.

  8. 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.

  9. K:PAPERSSPRINGBACK DESIGNPAPERSDM-PAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1498.pdf
    18 Feb 2002: 0 20 40 60 80 100 1200. 0.5. 1. 1.5. 2. ... 0 20 40 60 80 100 120 1400. 0.5. 1. 1.5.

  10. Space_Structures_Paper

    www-civ.eng.cam.ac.uk/dsl/publications/Space_Structures_Paper.pdf
    14 May 2002: θ = k 1( ) α2. γ12. γ22. (20). From this equation it can be seen that if the two reduction angles are equal, then the solutionis a line parallel to that of

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

    www-civ.eng.cam.ac.uk/dsl/publications/FoldableCompStruc.pdf
    15 Aug 2003: B, C Equal sense Outer 0.00 -1.26, 1.23 -1.20, 1.20Inner 0.00 1.02 -1.33 -1.27, 1.04.

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