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200 10$aComparison of NACA 0012 laminar flow solutions: structured and unstructured grid methods /$fR.C. Swanson, S. Langer
210  1$a[Hampton, VA] :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary 2016.
215   $a1 online resource (56 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-219003
300   $aTitle from title screen (viewed on June 1, 2016).
300   $a"January 2016."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (pages 25-27).
517   $aComparison of NACA 0012 laminar flow solutions
606   $aCompressible flow$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aComputational geometry$2nasat
606   $aLaminar flow$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aSteady state$2nasat
615  7$aCompressible flow.
615  7$aComputational fluid dynamics.
615  7$aComputational geometry.
615  7$aLaminar flow.
615  7$aNavier-Stokes equation.
615  7$aSteady state.
700   $aSwanson$b R. Charles$01401804
702   $aLanger$b S.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
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