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101   $aita
102   $aIT
105   $a|||| |||||
200 1 $a<<Le >> finanze dell'Europa$fDaniel Strasser
205   $aEd. riv. e ampliata
210   $aLussemburgo$cPubblicazioni ufficiali delle Comunita europee$d1982
215   $aXXIII, 445 p.$d25 cm
225  2$aProspettive europee
300   $aIn testa al front.: Commissione delle Comunita economiche europee.
410  1$12001$aProspettive europee
454  1$1001USA19404$12001$a<<Les>> finances de l'Europe$949160
606   $aComunità europee$2FI
620   $dLussemburgo
676   $a337.1$cCooperazione economica multilaterale$v21
700  1$aSTRASSER,$bDaniel$0122805
801   $aIT$bSOL$c20120104
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950   $aDIP.TO SCIENZE ECONOMICHE - (SA)$dDS 300 337.1 STR$e290 DISES
951   $a300 337.1 STR$b290 DISES
959   $aBK
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979   $c20121027$lUSA01$h1532
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979   $aPATRY$b90$c20121106$lUSA01$h1512
996   $aFinances de l'Europe$949160
997   $aUNISA
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100   $a20160809j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction /$fHyun D. Kim, Warren R. Hingst, and David O. Davis
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dDecember 1996.
215   $a1 online resource (9 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107392
300   $aTitle from title screen (viewed Aug. 9, 2016).
300   $a"December 1996"--Report documentation page.
300   $a"Prepared for the 35th Aerospace Sciences Meeting and Exhibit cosponsored by AIAA, ASME, SAE, and ASME, Reno, Nevada, January 6-10, 1997."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
300   $a"AIAA-97-0608."
320   $aIncludes bibliographical references (page 9).
606   $aBoundary layer control$2nasat
606   $aPressure measurement$2nasat
606   $aFlow visualization$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aMass flow rate$2nasat
606   $aStatic pressure$2nasat
606   $aShock waves$2nasat
615  7$aBoundary layer control.
615  7$aPressure measurement.
615  7$aFlow visualization.
615  7$aTurbulent boundary layer.
615  7$aMass flow rate.
615  7$aStatic pressure.
615  7$aShock waves.
700   $aKim$b Hyun Dae$01390070
702   $aHingst$b Warren R.
702   $aDavis$b David O.
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707497503321
996   $aExperimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction$93442386
997   $aUNINA