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020   $a2859390804
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035   $aPARLA209188$9ExL
040   $aDip.to Filosofia$bita
100 1 $aLefevre, Roger$0385780
245 13$aLa structure du Cartesianisme /$cRoger Lefevre
260   $aLille :$bPUL,$c1978
300   $a193 p. ;$c24 cm.
650  4$aCartesianismo
650  4$aDESCARTES, René
907   $a.b11365882$b02-04-14$c01-07-02
912   $a991000489759707536
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996   $aStructure du Cartesianisme$9816474
997   $aUNISALENTO
998   $ale005$b01-01-96$cm$da  $e-$feng$gfr $h3$i1

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100   $a20161013j199703    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEvaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight /$fScott R. Thomas, H. Douglas Perkins, and Charles J. Trefny
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dMarch 1997.
215   $a1 online resource (10 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107422
300   $a"March 1997"--Report documentation page.
300   $a"Prepared for the 89th Symposium sponsored by the Propulsion and Energetics Panel of the NATO Advisory Group for Aerospace Research and Development, Palaiseau, France, April 14-17, 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 4).
606   $aEjectors$2nasat
606   $aHydrocarbon fuels$2nasat
606   $aWind tunnel tests$2nasat
606   $aSupersonic speed$2nasat
606   $aMach number$2nasat
606   $aEngine tests$2nasat
606   $aPropulsion system performance$2nasat
606   $aFlow distribution$2nasat
615  7$aEjectors.
615  7$aHydrocarbon fuels.
615  7$aWind tunnel tests.
615  7$aSupersonic speed.
615  7$aMach number.
615  7$aEngine tests.
615  7$aPropulsion system performance.
615  7$aFlow distribution.
700   $aThomas$b Scott R.$01413894
702   $aPerkins$b H. Douglas
702   $aTrefny$b Charles J.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707625903321
996   $aEvaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight$93511516
997   $aUNINA