Search

Search Funnelback University

Search powered by Funnelback
1 - 10 of 19 search results for katalk:za33 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. 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. D:\Papers\Vibration wrinkled membranes SDM\SDM_Paper_2003.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Vibration_wrinkled_membranes_SDM.pdf
    14 Feb 2003: Mode 22 (41.81 Hz) Mode 23 (41.98 Hz) Mode 24 (44.32 Hz).
  4. C:\Documents and Settings\Sergio\My Documents\Papers\Wrinkled…

    www-civ.eng.cam.ac.uk/dsl/publications/Barcelonapaper.pdf
    24 Apr 2003: λ(δ1 δ2)π. (24). Here δ1 and δ2 are the radial displacements of the corners loaded by T1 and T2, respectively;these corner displacements can be estimated from. ... The wavelength predictions are very close.The wrinkle amplitudes have been estimated
  5. 28 Feb 2003: strains’ of Y 0:25% (suggested by the Eurocreteproject. 24), and Y 0:45% (proposed in ‘The Sheffield. ... 24. CLARKE J. L. and O’REGAN D. P. Design of concrete structures.
  6. 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.
  7. GROUND-BORNE VIBRATIONS DUE TO PILING OPERATIONS

    www-civ.eng.cam.ac.uk/geotech_new/people/bolton/mdb_pub/132_BGA_2003_743_756.pdf
    3 Mar 2003: 170 kW 27Hz vibrohammer. <6 (3 mm/s) 3.5 m 39.5 m 18.5 m 6-26 (2.3 mm/s) 4.5 m 51.5 m 24.1
  8. 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.
  9. Murphey et al AIAA-2003-1829 Traveler-ARM

    www-civ.eng.cam.ac.uk/dsl/publications/Murphey_AIAA_Traveler-ARM.pdf
    17 Feb 2003: α. α. =. =. (24). where I is the rotational inertia of a link. ... Again, the equation gives the average acceleration at time t. Equations (22) and (24) form a linear system of six equations with six unknowns.
  10. 1 Author’s contact details: R. J. Lock, Graduate Engineer, ...

    www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR320.pdf
    22 Jun 2003: 24 4.4 Field Study of an Integral Backwall Bridge: Hoppe & Gomez, 1996. ... 24. ntegral backwall bridge. he others presented in this report in that it is an integral.
  11. 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.

Refine your results

Search history

Recently clicked results

Recently clicked results

Your click history is empty.

Recent searches

Recent searches

Your search history is empty.