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001 9910705294603321
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035   $a(CKB)5470000002448416
035   $a(OCoLC)876159712
035   $a(EXLCZ)995470000002448416
100   $a20140409j201307    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA non-cut cell immersed boundary method for use in icing simulations /$fChristian M. Sarofeen and Ralph W. Noack, Richard E. Kreeger
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJuly 2013.
215   $a1 online resource (31 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2013-217881
300   $aTitle from title screen (viewed on Apr. 9, 2014).
300   $a"July 2013."
300   $a"Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012."
300   $a"AIAA-2012-1204."
320   $aIncludes bibliographical references (page 31).
606   $aAerodynamic coefficients$2nasat
606   $aAerodynamic drag$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aControl surfaces$2nasat
606   $aFinite volume method$2nasat
606   $aIce formation$2nasat
606   $aPressure distribution$2nasat
615  7$aAerodynamic coefficients.
615  7$aAerodynamic drag.
615  7$aComputational fluid dynamics.
615  7$aControl surfaces.
615  7$aFinite volume method.
615  7$aIce formation.
615  7$aPressure distribution.
700   $aSarofeen$b Christian M.$01415889
702   $aNoack$b Ralph W.
702   $aKreeger$b Richard E.
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705294603321
996   $aA non-cut cell immersed boundary method for use in icing simulations$93519292
997   $aUNINA