LEADER 01670nam 2200577 450 001 9910671124003321 005 20210104171433.0 010 $a85-361-9344-1 035 $a(CKB)4100000008521862 035 $a(MiAaPQ)EBC5758809 035 $a(EXLCZ)994100000008521862 100 $a20191210d2017 uy 0 101 0 $apor 135 $aurcnu|||||||| 181 $ctxt$2rdamedia/spa 182 $cc$2rdamedia/spa 183 $2rdacarrier/spa 200 10$aEstado covarde /$fWladimir Novaes Martinez 210 1$aSa?o Paulo :$cLTr Editora,$d2017. 215 $a1 recurso en li?nea (219 pa?ginas) 311 $a85-361-9244-5 320 $aContiene referencias bibliogra?ficas. 606 $aLaw$xPhilosophy 606 $aLaw$xPolitical aspects 606 $aState, The 606 $aPower (Social Sciences) 606 $aDerecho$xFilosofi?a 606 $aDerecho$xAspectos poli?ticos 606 $aEstado 606 $aPoder (Ciencias sociales) 608 $aLibros electronicos. 610 $aDireito--Filosofia 610 $aDireito e poli?tica 610 $aO Estado 610 $aPoder (Cie?ncias sociais) 615 0$aLaw$xPhilosophy. 615 0$aLaw$xPolitical aspects. 615 0$aState, The. 615 0$aPower (Social Sciences) 615 4$aDerecho$xFilosofi?a. 615 4$aDerecho$xAspectos poli?ticos. 615 4$aEstado. 615 4$aPoder (Ciencias sociales) 676 $a340.1 700 $aMartinez$b Wladimir Novaes$01335762 801 0$bFINmELB 801 1$bFINmELB 906 $aBOOK 912 $a9910671124003321 996 $aEstado covarde$93050654 997 $aUNINA LEADER 01505oam 2200445 450 001 9910717012003321 005 20220218115047.0 035 $a(CKB)5470000002528090 035 $a(OCoLC)1291212594 035 $a(OCoLC)995470000002528090 035 $a(EXLCZ)995470000002528090 100 $a20220106j199204 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model /$fAparajit J. Mahajan [and three others] 210 1$aWashington, D.C. :$cNASA,$dApril 1992. 215 $a1 online resource (approximately 14 pages) $cillustrations 225 1 $aNASA/TM ;$v105268 300 $a"April 1992." 320 $aIncludes bibliographical references (pages 6-7). 606 $aProp-fan technology$2nasat 606 $aFlutter$2nasat 606 $aCruise missiles$2nasat 615 7$aProp-fan technology. 615 7$aFlutter. 615 7$aCruise missiles. 700 $aMahajan$b Aparajit J$g(Aparajit Jagannath),$01419987 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 801 2$bGPO 801 2$bOCLCO 801 2$bGPO 906 $aBOOK 912 $a9910717012003321 996 $aAeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model$93536332 997 $aUNINA