LEADER 00985nam a2200289 i 4500
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005 20020507152511.0
008 000218s1993    it            ||| | ita  
020   $a8834830474
035   $ab11571597-39ule_inst
035   $aLE02726073$9ExL
040   $aDip.to Studi Giuridici$bita
082 0 $a321.6
084   $aC-XVII/A
100 1 $aDe Sanctis, Francesco M.$0437365
245 10$aDall'assolutismo alla democrazia /$cFrancesco M. De Sanctis
250   $a2. ed. riv. e ampliata
260   $aTorino :$bG. Giappichelli,$c[1993]
300   $a280 p. ;$c22 cm.
490 0 $aMulti Versum ;$v10
650  4$aAssolutismo$xTeorie
907   $a.b11571597$b01-03-17$c02-07-02
912   $a991001840019707536
945   $aLE027 C-XVII/A 130$g1$iLE027-1560$lle027$o-$pE0.00$q-$rl$s-  $t0$u0$v0$w0$x0$y.i11776304$z02-07-02
996   $aDall'assolutismo alla democrazia$9895594
997   $aUNISALENTO
998   $ale027$b01-01-00$cm$da  $e-$fita$git $h0$i1

LEADER 02339nam  2200613I  450 
001 9910702656103321
005 20141202152004.0
035   $a(CKB)5470000002429627
035   $a(OCoLC)897217438
035   $a(EXLCZ)995470000002429627
100   $a20141202j201406    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade /$fAshlie B. McVetta, Paul W. Giel, Gerard E. Welch
205   $aRevised copy.
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJune 2014.
215   $a1 online resource (23 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-218070/REV1
300   $aTitle from title screen (viewed Dec. 1, 2014).
300   $a"June 2014."
300   $a"This revised copy, numbered as NASA/TM-2013-218070/REV1, June 2014, supersedes the previous version, NASA/TM-2013-218070, August 2013, in its entirety."
300   $a"AIAA-2012-3879."
320   $aIncludes bibliographical references (page 23).
606   $aSupersonic turbines$2nasat
606   $aTurbine blades$2nasat
606   $aAerodynamic heat transfer$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aReynolds number$2nasat
606   $aPressure distribution$2nasat
606   $aInlet flow$2nasat
606   $aAngles (geometry)$2nasat
615  7$aSupersonic turbines.
615  7$aTurbine blades.
615  7$aAerodynamic heat transfer.
615  7$aComputational fluid dynamics.
615  7$aReynolds number.
615  7$aPressure distribution.
615  7$aInlet flow.
615  7$aAngles (geometry)
700   $aMcVetta$b Ashlie B.$01396822
702   $aGiel$b P. W$g(Paul W.),
702   $aWelch$b Gerard E.
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702656103321
996   $aAerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade$93457602
997   $aUNINA