LEADER 01842nam  2200505I  450 
001 9910702730803321
005 20150327154009.0
035   $a(CKB)5470000002430893
035   $a(OCoLC)905724843
035   $a(EXLCZ)995470000002430893
100   $a20150327j201409    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAFC-enabled simplified high-lift system integration study /$fPeter M. Hartwich [and seven others]
210  1$aHampton, Virginia. :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 2014.
215   $a1 online resource (v, 31 pages) $ccolor illustrations, maps
225 1 $aNASA/CR ;$v2014-218521
300   $aTitle from title screen (viewed March 27, 2015).
300   $a"September 2014."
320   $aIncludes bibliographical references (page 14).
517 3 $aActive Flow Control enabled simplified high lift system integration study
606   $aLift devices$2nasat
606   $aLeading edge slats$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aTrailing edge flaps$2nasat
606   $aDrooped airfoils$2nasat
615  7$aLift devices.
615  7$aLeading edge slats.
615  7$aAerodynamic characteristics.
615  7$aNavier-Stokes equation.
615  7$aTrailing edge flaps.
615  7$aDrooped airfoils.
700   $aHartwich$b Peter M.$01387208
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702730803321
996   $aAFC-enabled simplified high-lift system integration study$93451028
997   $aUNINA