LEADER 01940nam  2200469   450 
001 9910706551303321
005 20171201074453.0
035   $a(CKB)5470000002456934
035   $a(OCoLC)1013715980
035   $a(EXLCZ)995470000002456934
100   $a20171201j200104    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aGust acoustic response of a swept rectilinear cascade using the space-time CE/SE method /$fX.Y. Wang [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dApril 2001.
215   $a1 online resource (8 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210815
300   $a"April 2001."
300   $a"Prepared for the 2001 Fluids Engineering Division Summer Meeting sponsored by the American Society of Mechanical Engineers, New Orleans, Louisiana, May 29-June 1, 2001."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
300   $a"FEDSM 2001-18134."
320   $aIncludes bibliographical references (pages 3-4).
517 3 $aGust acoustic response of a swept rectilinear cascade using the space-time conservation element solution element method
606   $aAcoustics$2nasat
606   $aDynamic response$2nasat
606   $aNumerical analysis$2nasat
606   $aSound fields$2nasat
615  7$aAcoustics.
615  7$aDynamic response.
615  7$aNumerical analysis.
615  7$aSound fields.
700   $aWang$b X. Y.$01409484
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706551303321
996   $aGust acoustic response of a swept rectilinear cascade using the space-time CE$93523804
997   $aUNINA