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100   $a20131110j200103    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /$fDavid M. Schuster
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMarch 2001.
215   $a1 online resource (37 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210828
300   $a"March 2001."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 37).
606   $aTransonic wind tunnels$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aDynamic pressure$2nasat
606   $aStatic pressure$2nasat
606   $aViscous flow$2nasat
606   $aWind tunnel tests$2nasat
615  7$aTransonic wind tunnels.
615  7$aAerodynamic characteristics.
615  7$aDynamic pressure.
615  7$aStatic pressure.
615  7$aViscous flow.
615  7$aWind tunnel tests.
700   $aSchuster$b D. M$g(David M.),$01413984
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706548703321
996   $aAerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel$93511940
997   $aUNINA