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