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100   $a19921201d1550      uy             |
101 0 $aeng
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200 14$aThe vision of Pierce Plowman, nowe the seconde time imprinted by Roberte Crowley dwellynge in Elye rentes in Holburne. Whereunto are added certayne notes and cotations in the mergyne, geuynge light to the reader. And in the begynning is set a briefe summe of all the principall matters spoken of in the boke. And as the boke is deuided into twenty partes called passus: so is the summary diuided, for euery parte hys summarie, rehearsynge the matters spoken of in euerye parte, euen in suche order as they stande there$b[electronic resource]
210   $aImprinted at London $cBy [Richard Grafton for] Roberte Crowley, dwellyng in Elye rentes in Holburne$dThe yere of our Lord. M.D.L. [1550]
215   $a[8], Cxvii, [1] leaves
300   $aAttributed to William Langland.
300   $aIn verse.
300   $aThe B text.
300   $aActual printer's name from STC.
300   $aThe last leaf is blank.
300   $aReproduction of the original in the Henry E. Huntington Library and Art Gallery.
330   $aeebo-0113
700   $aLangland$b William$f1330?-1400?$0165667
801  0$bCu-RivES
801  1$bCu-RivES
801  2$bCStRLIN
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996   $aThe vision of Pierce Plowman, nowe the seconde time imprinted by Roberte Crowley dwellynge in Elye rentes in Holburne. Whereunto are added certayne notes and cotations in the mergyne, geuynge light to the reader. And in the begynning is set a briefe summe of all the principall matters spoken of in the boke. And as the boke is deuided into twenty partes called passus: so is the summary diuided, for euery parte hys summarie, rehearsynge the matters spoken of in euerye parte, euen in suche order as they stande there$92424598
997   $aUNISA

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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
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996   $aFinite element analysis and test results comparison for the hybrid wing body center section test article$93448981
997   $aUNINA