LEADER 01837nam  2200505I  450 
001 9910702672203321
005 20141009133217.0
035   $a(CKB)5470000002429465
035   $a(OCoLC)892640749
035   $a(EXLCZ)995470000002429465
100   $a20141009j201401    ua             0
101 0 $aeng
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