LEADER 01184nam a2200325 i 4500 001 991003674059707536 005 20021220115228.0 008 020410s2002 de ||| | eng 020 $a3540423052 035 $ab11846562-39ule_inst 035 $aLE01313146$9ExL 040 $aDip.to Matematica$beng 082 0 $a512.724 084 $aAMS 00A20 084 $aAMS 46L35 100 1 $aRordam, Mikael$0531783 245 10$aClassification of nuclear C*-algebras :$bentropy in operator algebras /$cM. Rordam, E. Stormer 260 $aBerlin :$bSpringer-Verlag,$cc2002 300 $avii, 198 p. ;$c25 cm 490 0 $aEncyclopaedia of mathematical sciences,$x0938-0396 ;$v126 490 0 $aOperator algebras and non-commutative geometry ;$v7 500 $aIncludes bibliographical references and index 650 0$aC*-algebras 700 1 $aStormer, Erling 907 $a.b11846562$b28-04-17$c20-12-02 912 $a991003674059707536 945 $aLE013 00A20 EMS11 V.126 (2002)$g1$i2013000133805$lle013$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i12098875$z20-12-02 996 $a-algebras$93371239 997 $aUNISALENTO 998 $ale013$b01-01-02$cm$da $e-$feng$gde $h0$i1 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