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102   $aIT
105   $aa---m--------
200 1 $aNumerical simulation of multi-dimensional hypersonic plasma flows$bTesi di dottorato$fDottorando: Raffaele Pepe$gCoordinatore: Vinicio Magi$gTutor: Aldo Bonfiglioli, Antonio D'Angola
210   $a[Potenza]$d[2015]
215   $aXX, 99 p.$cill.$d30 cm.
328  1$aTesi di dottorato: Università della Basilicata, Dottorato di ricerca in ingegneria industiale e dell'innovazione, XXVII ciclo, A.a. 2013-2014
676   $a621$v(22. ed.)$9Fisica applicata
686   $aING-IND/08$cMacchine a fluido
686   $aING-IND/18$cFisica dei reattori nucleari
700  1$aPepe,$bRaffaele$0447582
801  0$aIT$bUniversità della Basilicata - B.I.A.$gREICAT$2unimarc
912   $a000040700
996   $aNumerical simulation of multi-dimensional hypersonic plasma flows$9104762
997   $aUNIBAS
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100   $a20141009j201401    ua             0
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135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInvestigation of active flow control to improve aerodynamic performance of oscillating wings /$fRobert P. Narducci [and five others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary 2014.
215   $a1 online resource (vi, 66 pages) $cillustrations (some color)
225 1 $aNASA/CR ;$v2014-218146
300   $aTitle from title screen (viewed Oct. 9, 2014).
300   $a"January 2014."
320   $aIncludes bibliographical references (page 53).
606   $aAerodynamic stalling$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aActive control$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aRotary wing aircraft$2nasat
606   $aBoundary layer control$2nasat
606   $aMach number$2nasat
615  7$aAerodynamic stalling.
615  7$aComputational fluid dynamics.
615  7$aActive control.
615  7$aAerodynamic characteristics.
615  7$aRotary wing aircraft.
615  7$aBoundary layer control.
615  7$aMach number.
700   $aNarducci$b Robert P.$01385938
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702672203321
996   $aInvestigation of active flow control to improve aerodynamic performance of oscillating wings$93434417
997   $aUNINA