01720nam 2200601 a 450 991045776690332120200520144314.01-283-29975-597866132997580-19-161665-6(CKB)2550000000056206(SSID)ssj0000539413(PQKBManifestationID)12232749(PQKBTitleCode)TC0000539413(PQKBWorkID)10570944(PQKB)11435833(MiAaPQ)EBC975421(Au-PeEL)EBL975421(CaPaEBR)ebr10502887(CaONFJC)MIL329975(OCoLC)760886285(EXLCZ)99255000000005620620110622d2011 uy 0engurcn|||||||||txtccrNatural law and natural rights[electronic resource] /John Finnis2nd ed.Oxford ;New York Oxford University Press2011xvi, 494 pClarendon law seriesBibliographic Level Mode of Issuance: Monograph0-19-959914-9 0-19-959913-0 Includes bibliographical references (p. [480]-483) and index.Clarendon law series.Natural lawLawPhilosophyLaw and ethicsElectronic books.Natural law.LawPhilosophy.Law and ethics.Finnis John250551MiAaPQMiAaPQMiAaPQBOOK9910457766903321Natural Law and Natural Rights632533UNINA01891nam 2200553Ia 450 991070144970332120120308152323.0(CKB)5470000002418581(OCoLC)779542128(EXLCZ)99547000000241858120120308d2011 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierDesign, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners[electronic resource] /Wesley C.H. Slemp ... [and others]Hampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2011]1 online resource (39 pages) illustrations (some color)NASA/TP ;2011-217178Title from title screen (viewed on Mar. 8, 2012)."September 2011."Includes bibliographical references (pages 22-23).BucklingnasatFinite element methodnasatDesign optimizationnasatLoad testsnasatElastic bucklingnasatWing panelsnasatFixturesnasatDeflectionnasatLoads (forces)nasatBuckling.Finite element method.Design optimization.Load tests.Elastic buckling.Wing panels.Fixtures.Deflection.Loads (forces)Slemp Wesley C. H1407850Langley Research Center.GPOGPOBOOK9910701449703321Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners3490282UNINA