LEADER 02127nam  2200541   450 
001 9910706520903321
005 20171213082055.0
035   $a(CKB)5470000002457242
035   $a(OCoLC)1015309431
035   $a(EXLCZ)995470000002457242
100   $a20171213j199912    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSubsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration /$fBryan A. Campbell [and seven others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1999.
215   $a1 online resource (128 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209700
300   $a"December 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 128).
517 3 $aSubsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configuration
606   $aBoundary layer control$2nasat
606   $aLeading edges$2nasat
606   $aWind tunnel tests$2nasat
606   $aFlaps (control surfaces)$2nasat
606   $aPressure effects$2nasat
606   $aSubsonic speed$2nasat
606   $aSupersonic transports$2nasat
606   $aAerodynamic configurations$2nasat
615  7$aBoundary layer control.
615  7$aLeading edges.
615  7$aWind tunnel tests.
615  7$aFlaps (control surfaces)
615  7$aPressure effects.
615  7$aSubsonic speed.
615  7$aSupersonic transports.
615  7$aAerodynamic configurations.
700   $aCampbell$b Bryan A.$01395236
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706520903321
996   $aSubsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration$93539148
997   $aUNINA