LEADER 01662nam 2200421 450 001 9910703614903321 005 20150414125641.0 035 $a(CKB)5470000002433566 035 $a(OCoLC)907298619 035 $a(EXLCZ)995470000002433566 100 $a20150414d2014 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aTaxation $eforeign account tax compliance : agreement between the United States of America and Estonia, signed at Tallinn, April 11, 2014, with annexes 210 1$a[Washington, D.C.] :$cUnited States Department of State,$d[2014?] 215 $a1 online resource (51 unnumbered pages) 225 1 $aTreaties and other international acts series ;$v14-709 300 $aTitle from title screen (viewed on Apr. 14, 2015). 517 3 $aAgreement between the United States of America and Estonia, signed at Tallinn, April 11, 2014, with annexes 606 $aForeign bank accounts$xLaw and legislation$zEstonia 606 $aForeign bank accounts$xLaw and legislation$zUnited States 606 $aTax administration and procedure$xInternational cooperation 608 $aTreaties.$2lcgft 615 0$aForeign bank accounts$xLaw and legislation 615 0$aForeign bank accounts$xLaw and legislation 615 0$aTax administration and procedure$xInternational cooperation. 712 02$aUnited States.$bDepartment of State, 712 02$aEstonia, 712 02$aUnited States, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910703614903321 996 $aTaxation$9977289 997 $aUNINA LEADER 02470oam 2200685 450 001 9910716081503321 005 20210504085828.0 035 $a(CKB)5470000002517287 035 $a(OCoLC)785280935$z(OCoLC)495352125$z(OCoLC)495355007 035 $a(EXLCZ)995470000002517287 100 $a20120408j196812 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aHeat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K /$fby Jack G. Slaby and William F. Mattson 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1968. 215 $a1 online resource (ii, 22 pages) $cillustrations 225 1 $aNASA/TN ;$vD-4959 300 $a"December 1968." 320 $aIncludes bibliographical references (page 22). 606 $aCoefficients$2nasat 606 $aSurface temperature$2nasat 606 $aGas flow$2nasat 606 $aHoneycomb structures$xThermodynamics 606 $aNuclear fuel elements$xDesign and construction 606 $aNusselt number 606 $aGas flow$2fast 606 $aHeat$xTransmission$2fast 606 $aHoneycomb structures$xThermodynamics$2fast 606 $aHydrogen$xThermal properties$2fast 606 $aNuclear fuel elements$xDesign and construction$2fast 606 $aNusselt number$2fast 615 7$aCoefficients. 615 7$aSurface temperature. 615 7$aGas flow. 615 0$aHoneycomb structures$xThermodynamics. 615 0$aNuclear fuel elements$xDesign and construction. 615 0$aNusselt number. 615 7$aGas flow. 615 7$aHeat$xTransmission. 615 7$aHoneycomb structures$xThermodynamics. 615 7$aHydrogen$xThermal properties. 615 7$aNuclear fuel elements$xDesign and construction. 615 7$aNusselt number. 700 $aSlaby$b Jack G.$01400713 702 $aMattson$b William F. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bOCLCE 801 1$bOCLCE 801 2$bAD# 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910716081503321 996 $aHeat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K$93548218 997 $aUNINA