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100   $a20111002j199608    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aArtificial boundary conditions for computation of oscillating external flows /$fS.V. Tsynkov
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 1996.
215   $a1 online resource (43 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4714
300   $aTitle from title screen (viewed on Feb. 23, 2016).
300   $a"August 1996."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (pages 42-43).
606   $aBoundary conditions$2nasat
606   $aAirfoils$2nasat
606   $aFinite difference theory$2nasat
606   $aOscillating flow$2nasat
606   $aBoundary layers$2nasat
615  7$aBoundary conditions.
615  7$aAirfoils.
615  7$aFinite difference theory.
615  7$aOscillating flow.
615  7$aBoundary layers.
700   $aTsynkov$b Semyon V.$01399294
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910704399503321
996   $aArtificial boundary conditions for computation of oscillating external flows$93464231
997   $aUNINA