LEADER 01715nam  2200481   450 
001 9910706590103321
005 20171114110126.0
035   $a(CKB)5470000002456543
035   $a(OCoLC)1011358529
035   $a(EXLCZ)995470000002456543
100   $a20171113j200107    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAcoustical and flowfield characterization of a scaled tabletop rocket /$fMax Kandula [and three others]
210  1$aKennedy Space Center, Florida :$cNational Aeronautics and Space Administration, John F. Kennedy Space Center,$dJuly 2001.
215   $a1 online resource (v, 16 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210262
300   $a"July 2001".
300   $a"Performing organization: NASA John F. Kennedy Space Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 7-8).
606   $aAcoustics$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aRocket engines$2nasat
606   $aPressure oscillations$2nasat
606   $aFlow distribution$2nasat
606   $aCombustion products$2nasat
615  7$aAcoustics.
615  7$aComputational fluid dynamics.
615  7$aRocket engines.
615  7$aPressure oscillations.
615  7$aFlow distribution.
615  7$aCombustion products.
700   $aKandula$b Max$01399273
712 02$aJohn F. Kennedy Space Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706590103321
996   $aAcoustical and flowfield characterization of a scaled tabletop rocket$93464176
997   $aUNINA