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200 10$aVenus 2d vers in the Prize mus[i]ck$b[electronic resource] /$fcompos'd by Mr. J. Eccles, and sung by Mrs. Bracegirdle. T: Cross sculp
210   $a[London $cs.n.$dca. 1704]
215   $a1 score ([1] leaf)
300   $aSong from W. Congreve's masque, for voice and continuo (unfigured bass); with a version for the flute.
300   $aCaption title.
300   $aFirst line: Stay lovely youth delay thy choice.
300   $aEngraved throughout.
300   $aIn: A collection of songs by severall masters / [collected by] Francis Norton.
300   $aReproduction of the original in the British Library.
330   $aeebo-0018
606   $aSongs with continuo
606   $aIncidental music$vExcerpts
606   $aSongs, English
615  0$aSongs with continuo.
615  0$aIncidental music
615  0$aSongs, English.
700   $aEccles$b John$fd. 1735.$01004636
701   $aBracegirdle$b Anne$fca. 1663-1748.$01004637
701   $aCross$b Thomas$ffl. 1632-1682.$01003497
701   $aCongreve$b William$f1670-1729.$0163922
701   $aNorton$b Francis$01003498
801  0$bUMI
801  1$bUMI
801  2$bOCLCQ
801  2$bOCLCG
801  2$bUMI
906   $aBOOK
912   $a996394613503316
996   $aVenus 2d vers in the Prize musck$92319843
997   $aUNISA

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100   $a20180606j199804    ua             0
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEnergy efficient engine low pressure subsystem flow analysis /$fEdward J. Hall [and three others]
210  1$a[Cleveland, Ohio?] :$cNational Aeronautics and Space Administration, Lewis Research Center,$dApril 1998.
215   $a1 online resource (xv, 159 pages) $cillustrations
225 1 $aNASA/CR ;$v1998-206597
300   $a"April 1998."
320   $aIncludes bibliographical references (pages 101-111).
606   $aTurbofan engines$2nasat
606   $aTurbofans$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aRotor aerodynamics$2nasat
606   $aMathematical models$2nasat
615  7$aTurbofan engines.
615  7$aTurbofans.
615  7$aAerodynamic characteristics.
615  7$aRotor aerodynamics.
615  7$aMathematical models.
700   $aHall$b Edward J.$0121071
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709639903321
996   $aEnergy efficient engine low pressure subsystem flow analysis$93445385
997   $aUNINA