01507cam a2200301 a 4500991001023739707536110119s 000 0 ita d3039115170 9783039115174 b13948404-39ule_instDip.to Filologia Ling. e Lett.ita1583-2000 :quattro secoli di lessicografia italo-francese : repertorio analitico di dizionari bilingue /Jacqueline Lillo (ed.)Quattro secoli di lessicografia italo-francese :repertorio analitico di dizionari bilingueBern ;New York :Peter Lang,20082 v. (xxv, 1091 p.) :ill. ;24 cmInclude bibliografia ed indice Lingua italianaLessicografiaStoria Lingua FranceseLessicografiaStoria Lingua ItalianaDizionariFranceseBibliografiaLingua franceseDizionariItalianoBibliografia Lillo, Jacquelineauthorhttp://id.loc.gov/vocabulary/relators/aut731563.b1394840428-01-1419-01-11991001023739707536LE008 FL.M. (f.r.) XXIII 496 V. 1 12008000430474le008-E0.00-no 03030.i1522102719-01-11LE008 FL.M. (f.r.) XXIII 496 V. 2 12008000430481le008-E0.00-no 03130.i1522103919-01-111583-20001441274UNISALENTOle00819-01-11ma -itasz 0002926oam 2200637 450 991071601960332120210601091751.0(CKB)5470000002517912(OCoLC)23137432(OCoLC)761198139(EXLCZ)99547000000251791219910222j197211 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings /by Ralph L. Schacht, Harold G. Price, Jr., and Richard J. QuentmeyerWashington, D.C. :National Aeronautics and Space Administration,November 1972.1 online resource (41 pages) illustrationsNASA/TN ;D-7055"November 1972."Includes bibliographical references (page 18).An experimental investigation was conducted to determine the effective conductivities of four plasma-arc-sprayed, metal-ceramic gradated coatings on hydrogen-oxygen thrust chambers. The effective thermal conductivities were not a function of pressure or oxidant-to-fuel ratio. The various materials that made up these composites do not seem to affect the thermal conductivity values as much as the differences in the thermal conductivities of the parent materials would lead one to expect. Contact resistance evolving from the spraying process seems to be the controlling factor. The thermal conductivities of all the composites tested fell in the range of 0.75 to 7.5 watts per meter kelvin.Rocket firingnasatAeronauticsnasatCoatingsThermal propertiesTestingHeatTransmissionComposite materialsEffect of temperature onTestingRockets (Aeronautics)NozzlesHeatTransmissionfastRockets (Aeronautics)NozzlesfastRocket firing.Aeronautics.CoatingsThermal propertiesTesting.HeatTransmission.Composite materialsEffect of temperature onTesting.Rockets (Aeronautics)Nozzles.HeatTransmission.Rockets (Aeronautics)Nozzles.Schacht Ralph L.1397472Price Harold G.Quentmeyer Richard J.United States.National Aeronautics and Space Administration,ABCABCAD#OCLCEOCLCQOCLCOOCLCQOCLCFGPOBOOK9910716019603321Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings3459151UNINA