LEADER 01464nam2-2200433li-450 001 990000100190203316 005 20180312154758.0 035 $a0010019 035 $aUSA010010019 035 $a(ALEPH)000010019USA01 035 $a0010019 100 $a20001109d1975----km-y0itay0103----ba 101 0 $afre 102 $aFR 200 1 $aApplications de la thermodynamiquedu non-équilibre$ebases d'énergetique pratique$fPierre Chartier, Maurice Gross, K.S. Spiegler$gavant-propos par P. Glansdorff et I. Prigogine 210 $aParis$cHermann$d1975 215 $a191 p.$cill.$d24 cm 225 2 $aActualités scientifiques et industrielles$v1363 410 0$10010010020$12001$aActualités scientifiques et industrielles 610 1 $atermodinamica 676 $a5367$9. 700 1$aChartier,$bPierre$0223882 702 1$aGlansdorff,P 702 1$aGross,$bMaurice 702 1$aPrigogine I. 702 1$aSpiegler,$bK. S. 801 $aSistema bibliotecario di Ateneo dell' Università di Salerno$gRICA 900 1$aPrigogine$bIlya 912 $a990000100190203316 951 $a500 ASI (1363)$b0003401$c500$d00107512 959 $aBK 969 $aSCI 979 $c19900611 979 $c20001110$lUSA01$h1710 979 $aALANDI$b90$c20010510$lUSA01$h1003 979 $c20020403$lUSA01$h1617 979 $aPATRY$b90$c20040406$lUSA01$h1608 996 $aApplications de la thermodynamiquedu non-équilibre$91487614 997 $aUNISA LEADER 02286oam 2200649 450 001 9910717159703321 005 20220210084950.0 035 $a(CKB)5470000002528618 035 $a(OCoLC)1156323833 035 $a(EXLCZ)995470000002528618 100 $a20200602d1939 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aPressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight /$fby Th. Troller and F. Rokus 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939. 215 $a1 online resource (6 pages, 6 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 735 300 $a"November 1939." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 5). 606 $aAerodynamic load 606 $aAirplanes$xWings$xTesting 606 $aFlaps (Airplanes) 606 $aSplit flaps (Airplanes) 606 $aRolling (Aerodynamics) 606 $aYawing (Aerodynamics) 606 $aAerodynamic load$2fast 606 $aAirplanes$xWings$xTesting$2fast 606 $aFlaps (Airplanes)$2fast 606 $aRolling (Aerodynamics)$2fast 606 $aSplit flaps (Airplanes)$2fast 615 0$aAerodynamic load. 615 0$aAirplanes$xWings$xTesting. 615 0$aFlaps (Airplanes) 615 0$aSplit flaps (Airplanes) 615 0$aRolling (Aerodynamics) 615 0$aYawing (Aerodynamics) 615 7$aAerodynamic load. 615 7$aAirplanes$xWings$xTesting. 615 7$aFlaps (Airplanes) 615 7$aRolling (Aerodynamics) 615 7$aSplit flaps (Airplanes) 700 $aTroller$b T.$01414262 702 $aRokus$b Frank G. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910717159703321 996 $aPressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight$93529203 997 $aUNINA