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100   $a20160426j201512    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSecondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone /$fFei Li [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 2015.
215   $a1 online resource (24 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218997
300   $aTitle from title screen (viewed April 26, 2016).
300   $a"December 2015."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (pages 20-24).
606   $aBoundary layer flow$2nasat
606   $aCircular cones$2nasat
606   $aCross flow$2nasat
606   $aHypersonic boundary layer$2nasat
606   $aVortices$2nasat
615  7$aBoundary layer flow.
615  7$aCircular cones.
615  7$aCross flow.
615  7$aHypersonic boundary layer.
615  7$aVortices.
700   $aLi$b Fei$01406930
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707196303321
996   $aSecondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone$93487092
997   $aUNINA

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