LEADER 01597nam  2200457I  450 
001 9910707069903321
005 20160420130626.0
035   $a(CKB)5470000002460787
035   $a(OCoLC)946995482
035   $a(EXLCZ)995470000002460787
100   $a20160420j201512    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFlight tests of a supersonic natural laminar flow airfoil /$fMichael A. Frederick [and three others]
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration, Armstrong Flight Research Center,$dDecember 2015.
215   $a1 online resource (29 pages) $cillustrations
225 1 $aNASA/TM ;$v2015-218940
300   $aTitle from title screen (viewed April 20, 2016).
300   $a"December 2015."
320   $aIncludes bibliographical references (page 29).
606   $aBoundary layer transition$2nasat
606   $aChords (geometry)$2nasat
606   $aLaminar flow$2nasat
606   $aLeading edge sweep$2nasat
606   $aSupersonic airfoils$2nasat
615  7$aBoundary layer transition.
615  7$aChords (geometry)
615  7$aLaminar flow.
615  7$aLeading edge sweep.
615  7$aSupersonic airfoils.
700   $aFrederick$b Michael A.$01413784
712 02$aNASA Neil A. Armstrong Flight Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707069903321
996   $aFlight tests of a supersonic natural laminar flow airfoil$93516068
997   $aUNINA