LEADER 00996nam a2200265 i 4500 001 991003315619707536 005 20021205144722.0 008 020920s2001 us ||| | eng 020 $a0801022428 035 $ab11788689-39ule_inst 035 $aPARLA224335$9ExL 040 $aDip.to Filosofia$bita 082 0 $a230.044 100 1 $aAsselt, Willem J. : van$0530895 245 10$aReformation and Scholasticism :$ban ecumenical enterprise /$cedited by Willem J. van Asselt and Eef Dekker 260 $aGrand Rapids :$bBaker Academic 300 $a311 p. ;$c23 cm. 490 0 $aTexts and studies in Reformation and post-Reformation thought 700 1 $aDekker, Eef 907 $a.b11788689$b27-04-17$c09-12-02 912 $a991003315619707536 945 $aLE005 189 DEK01. 01$g1$i2005000132377$lle005$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i1203602x$z09-12-02 996 $aReformation and Scholasticism$9907818 997 $aUNISALENTO 998 $ale005$b01-01-02$cm$da $e-$feng$gus $h0$i1 LEADER 01678nam 2200457I 450 001 9910706249303321 005 20171018083920.0 035 $a(CKB)5470000002455945 035 $a(OCoLC)1006639218 035 $a(EXLCZ)995470000002455945 100 $a20171018j201604 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFinite element analysis and test results comparison for the hybrid wing body center section test article /$fAdam Przekop [and three others] 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2016. 215 $a1 online resource (viii, 106 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2016-218973 300 $a"April 2016." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 104-105). 606 $aCritical loading$2nasat 606 $aFinite element method$2nasat 606 $aStrain measurement$2nasat 606 $aStructural stability$2nasat 606 $aWings$2nasat 615 7$aCritical loading. 615 7$aFinite element method. 615 7$aStrain measurement. 615 7$aStructural stability. 615 7$aWings. 700 $aPrzekop$b Adam$01393174 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706249303321 996 $aFinite element analysis and test results comparison for the hybrid wing body center section test article$93448981 997 $aUNINA