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  2. Conceptual Design for a Laminar Flying Wing Aircraft

    www-g.eng.cam.ac.uk/advancedstructures/files/pdf/2009ConfAIAA.pdf
    7 Jul 2009: Conceptual Design for a Laminar Flying Wing Aircraft. T.I. Saeed , W.R. Graham†† , H. Babinsky ‡ , J.P. Eastwood , C.A. Hall , J.P. Jarrett ‖,. M.M. Lone and K.A. Seffen ††. Department of Engineering, University of Cambridge, Trumpington
  3. PII: S0925-9635(00)00479-9

    www-g.eng.cam.ac.uk/nms/publications/pdf/MilneDRM2001.pdf
    15 Oct 2009: Recently,a a. Ferrari and Robertson 24 have shown from their workŽ. ... Lett. 76. Ž. Ž. 18 2000 2627. Ž. 24 A.C. Ferrari, J.
  4. 3348:Regular Journal Pgs.qxd.qxd

    www-g.eng.cam.ac.uk/advancedstructures/files/pdf/2009AeroJ.pdf
    30 Oct 2009: The segmented primary reflector will consist of 18 hexagonalBeryllium (Be) 132m flat-to-flat segments, using heritagetechnology from the Spitzer mission(23,24).
  5. /home/journal/dvi/EPJD013-EPJD-final-print.dvi

    www-g.eng.cam.ac.uk/nms/publications/pdf/Milani_1999_EurPJD.pdf
    2 Feb 2009: All these parameters arein agreement with a more pronounced graphitic ordering ofthe sample [24]. ... Opt. 23, 3806 (1984)24. J. Robertson: Prog. Solid State Chem. 21, 199 (1991)25.
  6. Raman Spectroscopy of GrapheneEdgesC. Casiraghi,†,⊥ A. Hartschuh,‡ H. …

    www-g.eng.cam.ac.uk/nms/publications/pdf/Casiraghi_NanoLett2009.pdf
    8 Apr 2009: Thisis not due to increasing disorder, since in this case we expectFWHM(G) to increase,15 but it could be related to a dopingvariation,15,18,24 that is, this edge ... C. Solid State Commun. 2007, 143, 47.(24) Das, A.; Pisana, S.; Piscanec, S.; Chakraborty
  7. Plasma restructuring of catalysts for chemical vapor deposition of ...

    www-g.eng.cam.ac.uk/nms/publications/pdf/Cantoro_JAP2009.pdf
    24 Mar 2009: 064304-2 Cantoro et al. J. Appl. Phys. 105, 064304 2009. Downloaded 24 Mar 2009 to 129.169.178.169. ... J. Appl. Phys. 105, 064304 2009. Downloaded 24 Mar 2009 to 129.169.178.169.
  8. Subjecting a Graphene Monolayer to Tension and Compression

    www-g.eng.cam.ac.uk/nms/publications/pdf/Tsoukleri_small2009.pdf
    30 Oct 2009: stress transfer[24] and the fracture processes in unidirec-. tional,[25] but also multidirectional,[26] composites. ... H. Hong, Nature 2009, 457, 706.[24] N. Melanitis, C. Galiotis, Proc.
  9. st148018.dvi

    www-g.eng.cam.ac.uk/nms/publications/pdf/PiscanecEPJ2007.pdf
    15 Oct 2009: This is the Case in graphene, graphite and nanotubes, where γan is much smallerthan γEP [12].The EPC contribution to γqη is given by the Fermi golden rule [24]:. ... 94, 015503 (2005)24. P.B. Allen, Phys. Rev. B 6, 2577 (1972); P.B.
  10. was estimated to be 5 × 1016 m−2 on ...

    www-g.eng.cam.ac.uk/nms/publications/pdf/Elias_Science2009.pdf
    1 Feb 2009: Y. S. Li, N. R. Tao, K. Lu, Acta Mater. 56, 230 (2008).24. ... state by annealing (we used 450C in Ar atmo-sphere for 24 hours; higher annealing T dam-aged graphene).
  11. Nanotube-Polymer Composites for Ultrafast Photonics

    www-g.eng.cam.ac.uk/nms/publications/pdf/hasan_ADVMAT09.pdf
    20 Oct 2009: in order to induce a change inmaterial absorption or refractive index.[21–24] Each method hasits disadvantages. ... 1/e.[24] In general, for SAs, a high change in transmission isdesired between low and high power irradiation.[24] For SAs, a low.

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