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www.damtp.cam.ac.uk/user/ngb23/publications/nls1.pdf24 Sep 2002: "$#% &''()",))&,-. ()"/'1000. 24365873:9<;=7>243?587A@B5DCE;GF4HI9KJDFML3ONP@A5DQOCEFSRUTIVD;MWX@B3?5DYZ;GY[ 3:N8C7BY]3?_HV8abCEFXcdV8@NP@ Wfe. gihMjkhmlDnfoqprts. uwv)xzyB{}|Gv}q|1yA|/v}GyA|$/Av}{|6GtyA %A{qyB$fAKvv}Kty A{}/y=1A. < ¡ A¢£/ A¤D¥ -
Partial Differential Equations T. W. Körner after Joshi and ...
https://www.dpmms.cam.ac.uk/~twk/PDE.pdf12 Oct 2002: Lemma 1.1 (Proposition 1). If P and Q are linear partial differential op-erators. -
D:CURRENT_WORKWRINKLES COMPUTATIONSDM_2002_PAPERSDM-PAPER.DVI
www-civ.eng.cam.ac.uk/dsl/publications/AIAA2002-1369.pdf22 Mar 2002: geometries, numerical solutions are the only viable op-tion. The first finite element algorithm to incorporatewrinkling theory[12, 13] iteratively modified the mem-brane stiffness until all compressive stresses had beeneliminated. -
Deployable Tensegrity Structures for Space Applications
www-civ.eng.cam.ac.uk/dsl/publications/TibertDocThesis.pdf30 Jul 2002: TRITA-MEK Technical Report 2002:04 ISSN 0348-467XISRN KTH/MEK/TR--02/04--SE. Deployable Tensegrity Structuresfor Space Applications. Gunnar Tibert. Royal Institute of TechnologyDepartment of Mechanics. Doctoral ThesisStockholm, 2002. Deployable
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