LEADER 01567nam  2200457I  450 
001 9910703731303321
005 20150805083927.0
035   $a(CKB)5470000002434410
035   $a(OCoLC)915772179
035   $a(EXLCZ)995470000002434410
100   $a20150805j201411    ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDelay of transition using forced damping /$fReginald J. Exton
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 2014.
215   $a1 online resource (27 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218551
300   $aTitle from title screen (viewed Aug. 5, 2015).
300   $a"November 2014."
320   $aIncludes bibliographical references (page 10).
606   $aLeading edges$2nasat
606   $aBoundary layer transition$2nasat
606   $aBoundary layer stability$2nasat
606   $aDamping$2nasat
606   $aLaminar boundary layer$2nasat
615  7$aLeading edges.
615  7$aBoundary layer transition.
615  7$aBoundary layer stability.
615  7$aDamping.
615  7$aLaminar boundary layer.
700   $aExton$b Reginald J.$01416583
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703731303321
996   $aDelay of transition using forced damping$93522434
997   $aUNINA