LEADER 01018nam a22002651i 4500 001 991000100289707536 005 20031015104720.0 008 031111s1984 ru |||||||||||||||||eng 035 $ab12570497-39ule_inst 035 $aARCHE-060374$9ExL 040 $aDip.to Lingue$bita$cA.t.i. Arché s.c.r.l. Pandora Sicilia s.r.l. 082 04$a491.7 100 1 $aRassudova, Olga Petrovna$0458922 245 10$aAspectual usage in modern Russian /$cO.P. Rassudova 246 13$aUpotreblenie vidov glagola v sovremennom russkom jazyke (Titolo parallelo) 260 $aMoscow :$bRussky jazyk,$c1984 300 $a200 p. ;$c20 cm 500 $aFront. anche in russo 650 4$aLingua russa$xManuali 907 $a.b12570497$b02-04-14$c13-11-03 912 $a991000100289707536 945 $aLE012 491.78 RAS$g1$i2012000043961$lle012$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i13024863$z13-11-03 996 $aAspectual usage in modern Russian$9177017 997 $aUNISALENTO 998 $ale012$b13-11-03$cm$da $e-$feng$gru $h0$i1 LEADER 01805nam 2200433Ia 450 001 9910697023503321 005 20230902161938.0 035 $a(CKB)5470000002384670 035 $a(OCoLC)654839461 035 $a(EXLCZ)995470000002384670 100 $a20100811d2005 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 13$aAn optimal orthogonal decomposition method for Kalman filter-based turbofan engine thrust estimation$b[electronic resource] /$fJonathan S. Litt ; prepared for the Turbo Expo 2005 sponsored by the American Society of Mechanical Engineers, Reno, Nevada, June 6-9, 2005 210 1$aCleveland, Ohio :$cU.S. Army Research Laboratory, National Aeronautics and Space Administration, Glenn Research Center,$d[2005] 215 $a1 online resource (11 pages, 1 unnumbered page) $cillustrations 225 1 $aNASA/TM ;$v2005-213864 300 $aTitle from PDF title screen (NASA, viewed July 21, 2010). 300 $a"October 2005." 300 $a"ARL-TR-3487." 300 $a"GT2005-68808." 320 $aIncludes bibliographical references. 410 0$aNASA technical memorandum ;$v2005-213864. 606 $aAirplanes$xMotors$xThrust$xMeasurement$vCongresses 608 $aConference papers and proceedings.$2lcgft 615 0$aAirplanes$xMotors$xThrust$xMeasurement 700 $aLitt$b Jonathan S$01398039 712 02$aU.S. Army Research Laboratory. 712 02$aNASA Glenn Research Center. 712 12$aASME Turbo Expo. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910697023503321 996 $aAn optimal orthogonal decomposition method for Kalman filter-based turbofan engine thrust estimation$93535739 997 $aUNINA