LEADER 01887nam 2200589 450 001 9910461045903321 005 20200520144314.0 010 $a0-8047-9567-3 035 $a(CKB)3710000000411027 035 $a(MiAaPQ)EBC3568942 035 $a(Au-PeEL)EBL3568942 035 $a(CaPaEBR)ebr11055211 035 $a(OCoLC)932322643 035 $a(EXLCZ)993710000000411027 100 $a20150527h20152015 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $2rdacontent 182 $2rdamedia 183 $2rdacarrier 200 10$aDrugs, thugs, and diplomats $eU.S. policymaking in Colombia /$fWinifred Tate 210 1$aStanford, California :$cStanford University Press,$d2015. 210 4$dİ2015 215 $a1 online resource (300 pages) $cillustrations, photographs 225 1 $aAnthropology of Policy 311 $a0-8047-9566-5 311 $a0-8047-9201-1 320 $aIncludes bibliographical references and index. 410 0$aAnthropology of policy (Stanford, Calif.) 606 $aDrug control$zUnited States 606 $aDrug control$zColombia 606 $aMilitary assistance, American$zColombia 606 $aCounterinsurgency$zColombia 606 $aParamilitary forces$zColombia 607 $aUnited States$xForeign relations$zColombia 607 $aColombia$xForeign relations$zUnited States 607 $aColombia$xPolitics and government$y1974- 608 $aElectronic books. 615 0$aDrug control 615 0$aDrug control 615 0$aMilitary assistance, American 615 0$aCounterinsurgency 615 0$aParamilitary forces 676 $a327.730861 700 $aTate$b Winifred$f1970-$0975477 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910461045903321 996 $aDrugs, thugs, and diplomats$92221236 997 $aUNINA LEADER 02021oam 2200577Ka 450 001 9910698995003321 005 20090610112452.0 035 $a(CKB)5470000002397921 035 $a(OCoLC)384172382 035 $a(EXLCZ)995470000002397921 100 $a20090610d1989 ua 0 101 0 $aeng 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFeasibility and benefits of laminar flow control on supersonic cruise airplanes$b[electronic resource] /$fA.G. Powell, S. Agrawal, T. R. Lacey 210 1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[1989] 215 $a1 volume 225 1 $aNASA contractor report ;$v181817 300 $aTitle from title screen (viewed Jun. 9, 2009) 606 $aAerodynamic configurations$2nasat 606 $aBoundary layer control$2nasat 606 $aBoundary layer stability$2nasat 606 $aFeasibility analysis$2nasat 606 $aFighter aircraft$2nasat 606 $aLaminar boundary layer$2nasat 606 $aLaminar flow$2nasat 606 $aSupersonic aircraft$2nasat 606 $aSupersonic cruise aircraft research$2nasat 606 $aSupersonic transports$2nasat 615 7$aAerodynamic configurations. 615 7$aBoundary layer control. 615 7$aBoundary layer stability. 615 7$aFeasibility analysis. 615 7$aFighter aircraft. 615 7$aLaminar boundary layer. 615 7$aLaminar flow. 615 7$aSupersonic aircraft. 615 7$aSupersonic cruise aircraft research. 615 7$aSupersonic transports. 700 $aPowell$b A. G$01389264 701 $aAgrawal$b Sudhir$0515084 701 $aLacey$b T. R$01389265 712 02$aLangley Research Center. 801 0$bGPO 801 1$bGPO 801 2$bGPO 906 $aBOOK 912 $a9910698995003321 996 $aFeasibility and benefits of laminar flow control on supersonic cruise airplanes$93440557 997 $aUNINA