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- Date: 2002
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TR324
www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR324.pdf7 Oct 2002: 20 16 0.4m dia PSC hollow. Groups tied by beam. 1.0. ... 20 15 0.3m dia RCC hollow. Groups tied by beams. 1.0. -
The measurement of particle size distribution using the Single ...
www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR321.pdf20 Aug 2002: compared to sieving by 20-30%, as predicted by theoretical analysis. Measurements of. ... Isotropic compressionand shearing at 20.7 MPa. Isotropic compression to 62.1 MPa. -
Space_Structures_Paper
www-civ.eng.cam.ac.uk/dsl/publications/Space_Structures_Paper.pdf14 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 -
Publications / Presentations
www-civ.eng.cam.ac.uk/geotech_new/people/lynch/pubrl.html7 Mar 2002: 20. R J Lynch, G Measures and J T Hann, "The use of a practical interpretive solvent optimisation system in method development" presented at the Amsterdam International Chromatography Symposium, 1990. -
Press-in piling: Ground vibrations and noise during pile installation
www-civ.eng.cam.ac.uk/geotech_new/people/bolton/mdb_pub/117_DFC_2002_363_371.pdf6 Jun 2002: Air pressure, p (µPa) = 20 x 10(dB / 20) (1). ... 4. 20. 40. 60. 80. 100. 120. 140. 1 10 100 1000. -
poster
www-civ.eng.cam.ac.uk/dsl/wrinkling/poster_2002.pdf29 Jan 2002: 16. 18. 20. Shear angle, γ. λ (m. m). Eq. 10ABAQUSTest 1Test 2. -
LATERAL SPREADING OF SLOPES
www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR317.pdf28 Feb 2002: The final measured. ground displacement was 20 mm (1 m at prototype scale). ... 0. 20. 40. kPa. TEST SKH10. FLIGHT 1. Scales: Model. ShortTerm Time Records. -
LATERAL SPREADING OF SLOPES
www-civ.eng.cam.ac.uk/geotech_new/publications/TR/TR318.pdf4 Mar 2002: 10 PPT6672 256 122 5 PPT6675 380 190 50 PPT6679 200 130 20. ... 0. 10. 20. g. TEST SKH14. FLIGHT 1. Scales: Model. ShortTerm Time Records. -
K:PAPERSSPRINGBACK DESIGNPAPERSDM-PAPER.DVI
www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1498.pdf18 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. -
Deployable Tensegrity Structures for Space Applications
www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf30 Jul 2002: 42. Abbreviations. ACeS Asia Cellular Satellite, p. 20. ADAM Able Deployable Articulated Mast, p. ... 18. LaRC NASA Langley Research Center, p. 20. LDR Large Deployable Reflector, p.
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