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001 9910706132103321
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035   $a(CKB)5470000002455108
035   $a(OCoLC)858275004
035   $a(EXLCZ)995470000002455108
100   $a20130912j199912    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique /$fDanny P. Hwang
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 1999.
215   $a1 online resource (7 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209632
300   $a"December 1999."
300   $a"Prepared for the 38th Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 10-13, 2000."
300   $aPerforming organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
300   $a"AIAA-2000-0545."
320   $aIncludes bibliographical references (page 3).
606   $aSkin friction$2nasat
606   $aFriction reduction$2nasat
606   $aTurbulent flow$2nasat
606   $aSupersonic flow$2nasat
606   $aPorous plates$2nasat
615  7$aSkin friction.
615  7$aFriction reduction.
615  7$aTurbulent flow.
615  7$aSupersonic flow.
615  7$aPorous plates.
700   $aHwang$b Danny P.$01404710
712 02$aNASA Glenn Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706132103321
996   $aAn experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique$93541516
997   $aUNINA