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101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /$fBrenda E. Gile Laflin, Zachary T. Applin, and Kenneth M. Jones
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMarch 1997.
215   $a1 online resource (127 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110304
300   $a"March 1997."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (page 9).
606   $aAngle of attack$2nasat
606   $aMach number$2nasat
606   $aPressure distribution$2nasat
606   $aReynolds number$2nasat
606   $aSideslip$2nasat
606   $aSubsonic speed$2nasat
606   $aWings$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAngle of attack.
615  7$aMach number.
615  7$aPressure distribution.
615  7$aReynolds number.
615  7$aSideslip.
615  7$aSubsonic speed.
615  7$aWings.
615  7$aAerodynamic characteristics.
615  7$aWind tunnel tests.
700   $aLaflin$b Brenda E. Gile$01410731
702   $aApplin$b Zachary T.
702   $aJones$b Kenneth M.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707905303321
996   $aWind tunnel results of the aerodynamic performance of a 1$93500059
997   $aUNINA