LEADER 01831nam  2200481   450 
001 9910706120203321
005 20170914100726.0
035   $a(CKB)5470000002455228
035   $a(OCoLC)1003643373
035   $a(EXLCZ)995470000002455228
100   $a20170914j199912    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSubsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration /$fBryan A. Campbell [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1999.
215   $a1 online resource (103 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209701
300   $a"December 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 102-103 ).
606   $aSubsonic wind tunnels$2nasat
606   $aLeading edge flaps$2nasat
606   $aVortices$2nasat
606   $aSupersonic transports$2nasat
606   $aAerodynamic configurations$2nasat
606   $aSeparated flow$2nasat
615  7$aSubsonic wind tunnels.
615  7$aLeading edge flaps.
615  7$aVortices.
615  7$aSupersonic transports.
615  7$aAerodynamic configurations.
615  7$aSeparated flow.
700   $aCampbell$b Bryan A.$01395236
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706120203321
996   $aSubsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration$93453410
997   $aUNINA