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200 10$a100 ideas for assemblies $eprimary edition /$fFred Sedgwick
210  1$aLondon, [England] ;$aNew York, New York :$cContinuum,$d2011.
210  4$dİ2006
215   $a1 online resource (161 pages)
225 1 $aContinuum One Hundreds Series
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200 10$aAerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses /$fby Charles D. Harris
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dApril 1972.
215   $a1 online resource (55 pages) $cillustrations
225 1 $aNASA technical memorandum ;$vNASA TM X-2532
300   $aTitle from title screen (viewed on May 3, 2016).
300   $a"April 1972."
300   $a"Performing organization: NASA Langley Research Center, Hampton, Va."--Report documentation page.
320   $aIncludes bibliographical references (page 10).
606   $aAerodynamic characteristics$2nasat
606   $aSupercritical airfoils$2nasat
606   $aAirfoil profiles$2nasat
606   $aTransonic wind tunnels$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAerodynamic characteristics.
615  7$aSupercritical airfoils.
615  7$aAirfoil profiles.
615  7$aTransonic wind tunnels.
615  7$aWind tunnel tests.
700   $aHarris$b Charles D.$f1952-$01407191
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
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