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035   $aEXGIL134173$9ExL
040   $aBibl. Interfacoltà T. Pellegrino$bita$dSocioculturale Scs
041 0 $aita
082 04$a328.23$222
100 1 $aGrassi, Giuseppe$d<1883-1950>$01783810
245 13$aIl referendum nel governo di Gabinetto /$cGiuseppe Grassi
260   $aRoma :$bStab. Tip. Eredi A. Befani,$c1913
300   $a203 p. ;$c26 cm
650  4$aReferendum$zGran Bretagna
907   $a.b10610790$b02-04-14$c27-06-02
912   $a991004138799707536
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996   $aReferendum nel governo di Gabinetto$94312283
997   $aUNISALENTO
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100   $a20150429j201410    ua         0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aModeling the deterioration of engine and low pressure compressor performance during a roll back event due to ice accretion /$fJoseph P. Veres, Philip C.E. Jorgenson, and Scott M. Jones
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2014.
215   $a1 online resource (20 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218495
300   $aTitle from title screen (viewed on April 29, 2015).
300   $a"October 2014."
300   $a"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
320   $aIncludes bibliographical references (page 20).
606   $aEngine tests$2nasat
606   $aIce formation$2nasat
606   $aFlow velocity$2nasat
606   $aPropulsion system configurations$2nasat
606   $aThermodynamic cycles$2nasat
615  7$aEngine tests.
615  7$aIce formation.
615  7$aFlow velocity.
615  7$aPropulsion system configurations.
615  7$aThermodynamic cycles.
700   $aVeres$b Joseph P.$01386375
702   $aJorgenson$b Philip C. E$g(Philip Charles Eberhardt),
702   $aJones$b Scott M.
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703626303321
996   $aModeling the deterioration of engine and low pressure compressor performance during a roll back event due to ice accretion$93536456
997   $aUNINA