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1 - 10 of 21 search results for Economics middle test |u:www-civ.eng.cam.ac.uk where 0 match all words and 21 match some words.

  1. Results that match 2 of 3 words

  2. Deployable Tensegrity Structures for Space Applications

    www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf
    30 Jul 2002: A physicalmodel is built to analyse the feasibility of the concept and to test various deploy-ment schemes. ... A physicalmodel is built to analyse the feasibility of the concept and to test various deploymentschemes.

  3. Concrete Bridge Assessment Using Plastic Collapse Analysis

    www-civ.eng.cam.ac.uk/brg/papers/brgsrv98/
    29 Feb 2000: Values ranged from 0.87 in test A2 to 1.33 in test C2, with the range being between 1.04 and 1.33 for the first 11 tests. ... Hudson tests. Kite tests. Collins tests. Antill tests. Test No. H1.

  4. CUED home page - W Huang: actuator.html

    www-civ.eng.cam.ac.uk/dsl/sma/actuator.html
    21 Jul 1998: Several tests were carried out on this one-way actuator, both in the one-disk and three disk configurations. ... Working torques used in the test varied from -0.2 Nm to 0.62 Nm.

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

    www-civ.eng.cam.ac.uk/dsl/publications/New%20concepts.pdf
    17 Feb 2006: Displacement (mm). Fo. rce. (N. ). Test. Abaqus. Figure 12: Response to horizontal tip loads. ... Displacement (mm). Fo. rce. (N. ). Test. Abaqus. 6. Figure 13: Response to vertical tip loads.

  6. D:\Papers\Rigid Deployable Array TR\report.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/TR214.pdf
    7 Jul 2004: The measurements from two nominally identical tests, both beginning with the rotation set. ... root hinge has significant curvatures both near the clamps and in the middle.

  7. Tape Spring Large Deployable Antenna

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2006-1601-386.pdf
    11 May 2006: TOP SIDE. Figure 11. Test piece drawing (dimensions in mm). 7 of 12. ... First test-piece (a) hung for display (b) showing connectors at the back.

  8. D:CURRENT_WORKTSR HINGEPAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/TSR_hinge.pdf
    21 Jan 2002: A summary of allthe test results and analytical predictions is given in Table 1. ... The test results for the overall stiffness of thehinge in each component direction can be seen in Figure 7.

  9. D:CURRENT_WORKMEMBRANE VIBRATION IN AIRSDM PAPERSDM_PAPER.DVI

    www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1368.pdf
    18 Feb 2002: Theexperimental results presented in this reference are avery valuable benchmark against which to test new so-lutions. ... Comparison with Sewall’s Experiment. The third test case was based on one of the tests re-ported in Ref.

  10. D:\Current_work\Deployable_Reflector_Concept_SDM\Paper_SDM.dvi

    www-civ.eng.cam.ac.uk/dsl/publications/Reflector_concept_Paper.pdf
    29 Mar 2004: The tests were done with a cross-head speed of5 mm/min, and were recorded with a Sony DCR-PC110E digital video camera. ... Displacement (mm). Fo. rce. (N. ). Test. Abaqus. 6. Fig. 17 Response to vertical tip loads.

  11. Wrinkled membranesPart I: experiments

    www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p02-p.pdf
    23 Feb 2006: All test results presented in this section were obtained on 380 mm widemembranes with a height, between the supports, of 128 mm. ... Laser scanning frame. 3.2. Shear test apparatus. 3.3. Square membrane apparatus.

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