01097nam0-2200361---450-99001000622040332120151016145015.0978-88-299-2231-4001000622FED01001000622(Aleph)001000622FED0100100062220151016d2014----km-y0itay50------baitaengITNeuroanatomia attraverso casi cliniciHal Blumenfeld ;Edizione italianaa cura di Elena Pegoraro, Chiara Briani, Gianni SorarùPadovaPiccin2014XXIII, 1101 p.ill.29 cm2001Neuroanatomy through clinical casesAnatomia umanaSistema nervosoOrgani di senso611.823Blumenfeld,HalSorarù,GianniPegoraro,Elena<1958- >Briani,ChiaraITUNINARICAUNIMARCBK99001000622040332190 J 2c 1540/2015FMEBC90 J 2c 1641/2015FMEBCFMEBCUNINA01779nam 2200505I 450 991070481680332120131113164317.0(CKB)5470000002445571(OCoLC)862949255(EXLCZ)99547000000244557120131113d2013 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAdvanced shock position control for mode transition in a turbine based combined cycle engine inlet model /Jeffrey T. Csank and Thomas J. StueberCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2013]1 online resource (12 pages) illustrationsNASA/TM ;2013-216515Title from title screen (viewed Nov. 13, 2013)."May 2013."Includes bibliographical references (pages 11-12).Inlet flownasatControllersnasatFeedback controlnasatComputerized simulationnasatTurbine enginesnasatEngine inletsnasatInlet flow.Controllers.Feedback control.Computerized simulation.Turbine engines.Engine inlets.Csank Jeffrey T.1402819Stueber Thomas J.Fundamental Aeronautics Program (U.S.),NASA Glenn Research Center,GPOGPOBOOK9910704816803321Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model3512465UNINA