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100   $a20111115j198711    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aIntegration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /$fMilton Lamb, John R. Carlson, and Odis C. Pendergraft
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Division,$dNovember 1987.
215   $a1 online resource (21 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4018
300   $a"November 1987."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 3).
606   $aAngle of attack$2nasat
606   $aNacelles$2nasat
606   $aSeparated flow$2nasat
606   $aSupersonic flow$2nasat
606   $aTransonic wind tunnels$2nasat
615  7$aAngle of attack.
615  7$aNacelles.
615  7$aSeparated flow.
615  7$aSupersonic flow.
615  7$aTransonic wind tunnels.
700   $aLamb$b Milton$01393161
702   $aCarlson$b John R.
702   $aPendergraft$b Odis C.
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   $a9910707804103321
996   $aIntegration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport$93448935
997   $aUNINA