LEADER 00517nam0-22002291i-450- 001 990003091200403321 035 $a000309120 035 $aFED01000309120 035 $a(Aleph)000309120FED01 035 $a000309120 100 $a20000920d--------km-y0itay50------ba 101 0 $aita 102 $aIT 200 1 $aHayek$fGubeddu 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990003091200403321 952 $aPaper$fSES 959 $aSES 996 $aHayek$9459372 997 $aUNINA DB $aING01 LEADER 00811nam0-22003131i-450- 001 990003025790403321 035 $a000302579 035 $aFED01000302579 035 $a(Aleph)000302579FED01 035 $a000302579 100 $a20000920d1967----km-y0itay50------ba 101 0 $aita 102 $aIT 200 1 $aCGIL e politica agraria.. 210 $aRoma$cEditrice Sindacale Italiana$d1967. 215 $a42 p.$d21 cm 225 1 $aBrevi corsi sindacali$fCGIL$v3 610 0 $aAgricoltura$aItalia 610 0 $aSindacati$aItalia 676 $aG/2.43 676 $aH/1.124 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990003025790403321 952 $aH/1.124 CGI$b3087/I$fSES 959 $aSES 996 $aCGIL e politica agraria.$9467080 997 $aUNINA DB $aING01 LEADER 02284oam 2200661 450 001 9910716551403321 005 20210623121419.0 035 $a(CKB)5470000002522642 035 $a(OCoLC)23191302$z(OCoLC)761200313$z(OCoLC)785204937 035 $a(EXLCZ)995470000002522642 100 $a19910305j197210 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aApplication of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings /$fby Melvin H. Snyder, Jr., and John E. Lamar 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1972. 215 $a1 online resource (20 pages) $cillustrations 225 1 $aNASA/TN ;$vD-6994 300 $a"October 1972." 320 $aIncludes bibliographical references (pages 10-11). 606 $aAerodynamic loads$2nasat 606 $aDelta wings$2nasat 606 $aPitching (Aerodynamics) 606 $aAirplanes$xWings, Triangular 606 $aVortex-motion 606 $aAerodynamic load$2fast 606 $aAirplanes$xWings, Triangular$2fast 606 $aPitching (Aerodynamics)$2fast 606 $aVortex-motion$2fast 615 7$aAerodynamic loads. 615 7$aDelta wings. 615 0$aPitching (Aerodynamics) 615 0$aAirplanes$xWings, Triangular. 615 0$aVortex-motion. 615 7$aAerodynamic load. 615 7$aAirplanes$xWings, Triangular. 615 7$aPitching (Aerodynamics) 615 7$aVortex-motion. 700 $aSnyder$b Melvin H.$cJr,$f1921-$01395388 702 $aLamar$b John E. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 712 02$aLangley Research Center. 801 0$bABC 801 1$bABC 801 2$bAD# 801 2$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCF 801 2$bOCLCQ 801 2$bCOP 801 2$bGPO 906 $aBOOK 912 $a9910716551403321 996 $aApplication of the leading-edge-suction analogy to prediction of longitudinal load distribution and pitching moments for sharp-edged delta wings$93453827 997 $aUNINA