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101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aModifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment /$fCharles D. Harris and Cuyler W. Brooks
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Division,$dMay 1988.
215   $a1 online resource (120 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4032
300   $a"May 1988" Report documentation page.
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 6).
606   $aBoundary layer control$2nasat
606   $aHoneycomb structures$2nasat
606   $aLaminar boundary layer$2nasat
606   $aLinings$2nasat
606   $aPressure effects$2nasat
606   $aTest facilities$2nasat
606   $aTransonic wind tunnels$2nasat
615  7$aBoundary layer control.
615  7$aHoneycomb structures.
615  7$aLaminar boundary layer.
615  7$aLinings.
615  7$aPressure effects.
615  7$aTest facilities.
615  7$aTransonic wind tunnels.
700   $aHarris$b Charles D.$f1952-$01407191
702   $aBrooks$b Cuyler W.$cJr.,
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Division,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707801703321
996   $aModifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment$93487888
997   $aUNINA