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200 10$aGodlinesse in principle and conversation$b[electronic resource] $ea necessary preparative to the worlds dissolution and the escaping of future burnings /$fby Thomas Vincent ..
210   $aLondon $cPrinted for George Calvert and Sam. Sprint ...$d1670
215   $a48 p
300   $aThe copy at reel position 1217:15 is an improved filming of the copy at reel position 1106:19.
300   $aReproduction of original in the Union Theological Seminary Library, New York.
330   $aeebo-0160
606   $aJudgment Day
606   $aApocalyptic literature
615  0$aJudgment Day.
615  0$aApocalyptic literature.
700   $aVincent$b Thomas$f1634-1678.$01001065
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan$b[electronic resource] /$fGregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011]
215   $a1 online resource (14 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-216959
300   $aTitle from title screen (viewed on June 27, 2011).
300   $a"January 2011."
300   $a"AIAA-2010-6711."
320   $aIncludes bibliographical references (pages 13-14).
606   $aAeroelasticity$2nasat
606   $aTurbomachinery$2nasat
606   $aTurbofans$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aInlet flow$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aHigh speed$2nasat
615  7$aAeroelasticity.
615  7$aTurbomachinery.
615  7$aTurbofans.
615  7$aComputational fluid dynamics.
615  7$aInlet flow.
615  7$aAerodynamic characteristics.
615  7$aHigh speed.
700   $aHerrick$b Gregory Paul$f1972-$01387242
712 02$aFundamental Aeronautics Program (U.S.)
712 02$aNASA Glenn Research Center.
712 12$aAIAA/ASME/SAE/ASEE Joint Propulsion Conference$d(46th :$f2010 :$eNashville, Tenn.)
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