00867nam0-2200289---450-99000846913040332120070215123824.0000846913FED01000846913(Aleph)000846913FED0100084691320070215d1976----km-y0itay50------baitaIT--------001yyPatres conscriptiun'ipotesi sulla composizione dell'antico senato romanoGaetano MancusoPalermoMontaina1976P. 254-28824 cmEstratto da: Annali del Sem. Giuridico di Palermo, vol. XXXVIMancuso,Gaetano291260ITUNINARICAUNIMARCBK990008469130403321DDR(E)-Mancuso-1976.1Estr. 11 ddrDDRDDRPatres conscripti729617UNINA01940oam 2200517I 450 991071386230332120200828095402.0(CKB)5470000002505070(OCoLC)1136490240(EXLCZ)99547000000250507020200116d1929 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind tunnel pressure distribution tests on a series of biplane wing modelsPart IEffects of changes in stagger and gap /by Montgomery Knight and Richard W. NoyesWashington, [D.C.] :National Advisory Committee for Aeronautics,1929.1 online resource (13 pages, 20 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 310"July, 1929."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 13).Effects of changes in stagger and gapAirplanesWingsDesign and constructionWind tunnel testingBiplanesAirplanesWingsDesign and constructionfastWind tunnel testingfastAirplanesWingsDesign and construction.Wind tunnel testing.Biplanes.AirplanesWingsDesign and construction.Wind tunnel testing.Knight Montgomery1390967Noyes Richard W.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713862303321Wind tunnel pressure distribution tests on a series of biplane wing models3444189UNINA