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101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$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,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707148103321
996   $aAerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses$93531555
997   $aUNINA