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200 1 $aJocelyn$fAlphonse de Lamartine$gnotes par Claude Jorry
210   $aParis$cLarousse$d1953
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101 0 $aeng
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181   $ctxt$2rdacontent
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200 10$aCFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report /$fSamuel J. Vinci
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dSeptember 2012.
215   $a1 online resource (xiv, 113 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2012-217417
300   $aTitle from title screen (viewed Nov. 24, 2015).
300   $a"September 2012."
300   $a"Performing organization: Cleveland State University"--Report documentation page.
300   $a"Prepared under NASA interagency agreement no. NNC07IA10I (through U.S. Navy Agreement No. N00189-07-P-A253)."
320   $aIncludes bibliographical references (pages 110-113).
517   $aCFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil 
606   $aComputational fluid dynamics$2nasat
606   $aPressure ratio$2nasat
606   $aBoundary layers$2nasat
606   $aFinite volume method$2nasat
606   $aLow speed wind tunnels$2nasat
615  7$aComputational fluid dynamics.
615  7$aPressure ratio.
615  7$aBoundary layers.
615  7$aFinite volume method.
615  7$aLow speed wind tunnels.
700   $aVinci$b Samuel J.$01423048
712 02$aCleveland State University.
712 02$aFundamental Aeronautics Program (U.S.),
712 02$aNASA Glenn Research Center,
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