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TechRep_1.dvi
www-civ.eng.cam.ac.uk/dsl/publications/CRTS_vibration.pdf26 Mar 2001: ModeFrequency (Hz). 6 ribs 12 ribs 24 ribs. 1 16.46 17.78 17.40. ... ModeFrequency (Hz). 6 ribs 12 ribs 24 ribs. 1 3.14 2.97 2.85. -
CUED Bridge Research - Publications
www-civ.eng.cam.ac.uk/brg/papers/29 Sep 2004: 1997. Middleton, C.R. Concrete bridge assessment: an alternative approach. The Structural Engineer, Vol.75 No.23&24, 9th December 1997, pp.403-409. -
Chris Morley
www-civ.eng.cam.ac.uk/struct/ctm/publications.html30 Nov 2007: Magazine of Concrete Research. Special Publication on Recent Developments in Yield Line Theory, 13-24. -
Cambridge University Engineering Dept. - Structures Group
www-civ.eng.cam.ac.uk/crc/crc.pubs.htm11 Jan 2000: J. Mech. Sci., 24, 219-230 (1982). 57. C.R. Calladine, 'Modal stiffnesses of a pre-tensioned cable net', Int. ... 110. C.R. Calladine, "Some paradoxical experiments on beams". International Journal of Mechanical Engineering Education, 24, 37-48 (1996). -
Publications / Presentations
www-civ.eng.cam.ac.uk/geotech_new/people/lynch/pubrl.html7 Mar 2002: Unicam Application note. 24. N Perez-Souto, R J Lynch, G Measures and J T Hann, " Use of high performance liquid chromatographic peak deconvolution and peak labelling to identify antiparasitic components -
D:CURRENT_WORKMEMBRANE VIBRATION IN AIRSDM PAPERSDM_PAPER.DVI
www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1368.pdf18 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. -
Concrete Bridge Assessment Using Plastic Collapse Analysis…
www-civ.eng.cam.ac.uk/brg/papers/brgsrv98/plaintbl.html12 Aug 1998: Hudson tests Kite tests Test No. H1 H2 H3 H4 K1 K2 K3 K4 Ptest (kN) 29.2 28.3 27.9 19.0 23.4 23.5 24.1 ... 7 PCOBRAS (kN) 24.5 25.3 23.0 17.2 22.5 22.3 20.5 17.7 Ptest/PCOBRAS 1.19 1.12 1.21 1.10 1.04 -
Matthew DeJong - Publications
www-civ.eng.cam.ac.uk/struct/mjd/publications.html10 Jan 2017: DeJong MJ, De Lorenzis L, Adams S, Ochsendorf JA (2008). Rocking stability of masonry arches in seismic regions, Earthquake Spectra, 24(4), 847-865. -
CUED home page - W Huang: actuator.html
www-civ.eng.cam.ac.uk/dsl/sma/actuator.html21 Jul 1998: 24 mm, i.d. 9 mm). In order to insulate both electrically and thermally the Nitinol wire from the steel disk, a series of Macor cylinders with 1.1 mm diameter -
Department of Engineering - Bridge Research Group - Publications
www-civ.eng.cam.ac.uk/brg/publications.html22 Dec 2011: In Proceedings of the Annual International fib Symposium Concrete : 21st Century Superhero, Building a sustainable future, held in London, 22-24 June 2009. ... In Foundations: proceedings of the second British Geotechnical Association international -
Cam Middleton: Publications
www-civ.eng.cam.ac.uk/struct/crm/publications.html27 May 2011: In Proceedings of the Annual International fib Symposium Concrete : 21st Century Superhero, Building a sustainable future, held in London, 22-24 June 2009. ... 1997. Middleton, C.R. Concrete bridge assessment: an alternative approach. The Structural -
E:CURRENT_WORKTENSEGRITY_FORM-FINDINGPAPER.DVI
www-civ.eng.cam.ac.uk/dsl/publications/tensegrity.pdf2 Apr 2001: E(p) =12pT. . p, (24). where the elements of are given by. ... Proceedings of Cold Spring Harbor Symposium on Quantitative Biology, 1962, 27, 1-24. -
Chris Calladine
www-civ.eng.cam.ac.uk/struct/crc/publications.html21 Aug 2008: J. Mech. Sci., 24, 219-230 (1982). 57. C.R. Calladine, 'Modal stiffnesses of a pre-tensioned cable net', Int. ... 110. C.R. Calladine, "Some paradoxical experiments on beams". International Journal of Mechanical Engineering Education, 24, 37-48 (1996). -
Concrete Bridge Assessment Using Plastic Collapse Analysis
www-civ.eng.cam.ac.uk/brg/papers/brgsrv98/29 Feb 2000: Assistant Director of Research, University of Cambridge, U.K. First presented at the Bridge Surveyor Conference, 24. ... A2. P. test. (kN). 29.2. 28.3. 27.9. 19.0. 23.4. 23.5. 24.1. -
E:CURRENT_WORKCRTS DEMONSTRATORREPORT.DVI
www-civ.eng.cam.ac.uk/dsl/publications/CRTS2001.pdf21 Mar 2001: 50 mm. 85 mm. Figure 3.4: Cylindrical mould. 22 23 24 25 26 27 28 29 30 31 3216. ... 17. 18. 19. 20. 21. 22. 23. 24. Rm [mm]. Rr[mm] Rr = 0.4957Rm 6.7181. -
IStructE 2003 Poster
www-civ.eng.cam.ac.uk/dsl/ppao2/documents/IStructE_2003_Poster.pdf22 May 2003: 4 8 12 16 20 24 28 32 36 401.0. 1.1. -
paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/balloons.pdf8 Feb 2000: 24. L2. h2B. 2(15). and. v =h 2. 24. L2. h2 B. ... u v = 2. h 2. 24. L. h. 2(19). u2 v2 =. h 2. 24. 2 L. h. 4B2 2. 4(20). Substituting back into Equation 18, ignoring higherorder terms, and -
C:\Documents and Settings\Sergio\My Documents\Papers\Wrinkled…
www-civ.eng.cam.ac.uk/dsl/publications/Barcelonapaper.pdf24 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 -
E:CURRENT_WORKCRTS TECHNOLOGYREPORT.DVI
www-civ.eng.cam.ac.uk/dsl/publications/TR195.pdf5 Apr 2001: Configuration 12 13.4. 24 3.6. Circular 6 45.9. Configuration 12 12.5. ... apertures of 1, 3, 5, and 10 m, with 6, 12, and 24 ribs. -
report1.dvi
www-civ.eng.cam.ac.uk/dsl/publications/TR170.pdf21 Mar 2001: TB =. 1. 24. 24b1 0 b2 0 b3 00 c1 0 c2 0 c3c1 b1 c2 b2 c3 b3. ... Figure 3.2: Equilibrium surface. 24. 0.2 0.1 0 0.1 0.2. 0.1. -
Computation of Buckling Pressure of Pumpkin Balloons
www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2006-1803-983.pdf11 May 2006: n 16-48 64-96 112-145Elements along tendons 100 116 134Elements at equator 30 24 20Number of elements 3460 3216 3072Number of nodes 1831 1725 1671. ... Figures 24(a) and 24(b) show this type ofplot respectively for nCA118-10-290 and nCR118-10-290 balloons -
D:\Papers\Low-cost hinge report\report.dvi
www-civ.eng.cam.ac.uk/dsl/publications/report.pdf12 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. -
Murphey and Pellegrino, NEM, AIAA-2004-1528, Rev 10
www-civ.eng.cam.ac.uk/dsl/publications/Actuated_tape_spring_SDM.pdf19 Apr 2004: cossin. ψψ. =. b (24). where ψ is the angular orientation of b and ranges π. ... Expanding Equation (23) with Equation (24) and writing the result in matrix form gives the stiffness in the ψ direction TKψ = b Kb (25) where. -
Murphey et al AIAA-2003-1829 Traveler-ARM
www-civ.eng.cam.ac.uk/dsl/publications/Murphey_AIAA_Traveler-ARM.pdf17 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. -
E:CURRENT_WORKDERA PROJECTSMALL SATELLITE MECHANISMSREPORT.DVI
www-civ.eng.cam.ac.uk/dsl/publications/TR190.pdf17 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. -
C:\Documents and Settings\Sergio\My…
www-civ.eng.cam.ac.uk/dsl/publications/Space-Frames_SDM_paper.pdf30 Mar 2004: W = PE δwsin2θcosθ. (23). But, since. φ =π. 2 2θ (24). -
University of Cambridge Department of Engineering Vibration of…
www-civ.eng.cam.ac.uk/dsl/publications/KukaMPhil.pdf25 Sep 2000: 4.8 Mode shapes of 10 m diameter re ector with 24 ribs. ... 24. 3.2. SIMPLE MEMBRANE STRUCTURE. Table 3.5: Natural frequencies of simple structure. -
SDM2003_1978.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Deployable_tensegrity_masts.pdf28 Feb 2003: Pak. Deployable tensegrity structures.Fourth-year undergraduate project report, 24 May2000. Department of Engineering, University ofCambridge, Cambridge, UK. -
Topology Optimization of Adaptive Compliant Aircraft Wing Leading…
www-civ.eng.cam.ac.uk/dsl/publications/topology_paper_SDM.pdf2 Apr 2007: 24–33.3“SAMCEF v12.0-03,” Samtech Group, LIEGE science park, Rue des Chasseurs-Ardennais, 8B-4031 Liège (Angleur),. -
Thin-Shell Deployable Reflectors with Collapsible Stiffeners: Part I…
www-civ.eng.cam.ac.uk/dsl/publications/Reflectors-with-stiffeners.pdf1 Mar 2005: C90 2.72 24.76 4.18 39.18 0.274. Table 3. Comparison of optimized Configuration D. ... 24 of 28. Tan & Pellegrino. of given width and thickness, shortening the slits at the end of diameter d1 increases the. -
Modelling of Anisotropic Viscoelastic Behaviour in Super-Pressure…
www-civ.eng.cam.ac.uk/dsl/publications/Anisotropic%20viscoelastic%20behaviour.pdf10 Apr 2007: 40 -20 0 2002468. 10. Temperature [oC]. Log a. T. 0 4 8 12 16 20 24. -
Murphey and Hinkle, Hierarchical Space Structures AIAA 200–
www-civ.eng.cam.ac.uk/dsl/publications/HierarchicalSpaceStructures.pdf23 Apr 2003: π= (24). The battens and diagonals must provide enough support to the longerons to enforce local buckling. -
SDM04.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Ultrathin_antennas_Paper.pdf31 Mar 2004: Resulting in λ = 7.11 104and a corresponding fundamental natural frequency of0.24 Hz.†. -
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.pdf14 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. -
D:\Papers\Bistable prestressed shells\Paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Kebadze-Guest-Pellegrino_revised.pdf17 Feb 2004: 4Test. -4-21 23 -24. Analysis -26 24 -26. 5Test. -3.2-18 36 -22. ... shell; the configurations (b-d) are unstable. 24. Figure 3: Sliced-up shell. -
D:\Papers\Amplitude_of_wrinkles\paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/amplitude_of_wrinkles.pdf3 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. -
Viscoelastic Behaviour of Pumpkin Balloons T. Gerngross, Y. Xu ...
www-civ.eng.cam.ac.uk/dsl/publications/viscoelastic%20behaviour%20of%20pumpkin%20balloons.pdf17 Apr 2007: 0 4 8 12 16 20 24. -1.2. -0.8. -0.4. 0.0. -
Wrinkled membranesPart II: analytical models
www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p03-p.pdf23 Feb 2006: 12(1 ν2)π 4 A2. 4λ4. (24). The stretching strain energy per unit area can be obtained, neglecting stretchingin the η-direction, from. ... U =(1 ν)E t γ. 2. (π 2t 2. 24(1 ν2)λ2+. -
Optimization pumpkin balloons.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Optimization%20pumpkin%20balloons%20SMALL.pdf7 May 2007: l = an1 anb. (23). Therefore,. a =1 5. 2; b =. 3 52. (24). and hence. τ =a. b=. 1 53 5 =. 1. 52. = 1.618033989. (25). is the golden ratio.As -
D:\Current_work\Stiffened Springback ESTEC\paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/springback_paper.pdf27 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. -
D:\Papers\Vibration wrinkled membranes SDM\SDM_Paper_2003.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Vibration_wrinkled_membranes_SDM.pdf14 Feb 2003: Mode 22 (41.81 Hz) Mode 23 (41.98 Hz) Mode 24 (44.32 Hz). -
Deployable Tensegrity Structures for Space Applications
www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf30 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 -
report_final.dvi
www-civ.eng.cam.ac.uk/dsl/publications/TR192.pdf21 Mar 2001: 2.24). wherefromYoung(1989p.68). I x. =. R3t. 1. 3t 2R+. t2 R2. ... The transformation of the nodal coordinates is2. 4XYZ. 35 =. 24 cos sin 0sin cos 0. -
E:/Diplomarbeit/Latex/Thesis.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Schultheiss_Diploma_paper.pdf12 Nov 2003: 24. 3.13 Example of two Non-holonomic Restrictions Being Violated and its Handling. ... Time. 41. 3.24 Force of Static Friction vs. Normal Force. 41. -
D:\Current_work\Closed-Loop Linkages\SDM_paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/Closed-loops_SDM.pdf14 Feb 2003: weobtain. T1TĀT3TB̄T1TC̄T3TD̄. (T1UĀT3TB̄T1TC̄T3TD̄) θ′A+(T1TĀT3UB̄T1TC̄T3TD̄) θ′B+(T1TĀT3TB̄T1UC̄T3TD̄) θ′C+(T1TĀT3TB̄T1TC̄T3UD̄) θ′D = I (24). From Equation 23, the first term in Equation 24 isequal to I E. -
Mapping two-way grids onto free-form surfaces P. Winslow S. ...
www-civ.eng.cam.ac.uk/dsl/publications/Mapping_two-way_grids.pdf20 Jul 2007: α25 and β1, β2,. β25.However, only 24 design variables are needed to represent each grid design, due to symmetry anddue to a more advanced parameter smoothing process. ... Loading 1 kPa pressure loadingNumber of regions 25Number of design variables -
D:\Current_work\CRTS Reflectors\paper.dvi
www-civ.eng.cam.ac.uk/dsl/publications/CRTS_paper.pdf27 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. -
March 12, 2003 11:8 Proceedings of OMAE’0322nd International…
www-civ.eng.cam.ac.uk/dsl/publications/OMAE2003-37465.pdf14 Mar 2003: e11 =h1A2 h2A1. (h1h3 h22)|V |(23). e12 =h3A1 h2A2. (h1h3 h22)|H|(24). ... At this. 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 401. -
C:DOCUMENTS AND SETTINGSADMINISTRATORMY…
www-civ.eng.cam.ac.uk/dsl/publications/tensereflect.pdf10 Nov 2001: b = 2 (15 6) 24 = 204 (5). Substituting Equations 4 and 5 into Equation 1 we obtain. ... 8. Figure 12: Variation of forces in net cables. 24. 0 5 10 15 20 25 303.5.
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