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101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aUse of constrained optimization in the conceptual design of a medium-range subsonic transport /$fSteven M. Sliwa
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1980.
215   $a1 online resource (35 pages) $cillustrations
225 1 $aNASA technical paper ;$v1762
300   $aTitle from title screen (viewed on Aug. 18, 2016).
300   $a"December 1980."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 18-20).
606   $aAerodynamic configurations$2nasat
606   $aCost analysis$2nasat
606   $aDesign analysis$2nasat
606   $aOptimization$2nasat
606   $aTransport aircraft$2nasat
615  7$aAerodynamic configurations.
615  7$aCost analysis.
615  7$aDesign analysis.
615  7$aOptimization.
615  7$aTransport aircraft.
700   $aSliwa$b Steven M.$01422208
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707458603321
996   $aUse of constrained optimization in the conceptual design of a medium-range subsonic transport$93545768
997   $aUNINA