LEADER 01882nam  2200493I  450 
001 9910704910603321
005 20140821161547.0
035   $a(CKB)5470000002446644
035   $a(OCoLC)888236259
035   $a(EXLCZ)995470000002446644
100   $a20140821d2013      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExhaust nozzle plume and shock wave interaction /$fRaymond S. Castner, Alaa Elmiligui, Susan Cliff
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2013.
215   $a1 online resource (21 pages) $cillustrations
225 1 $aNASA/TM ;$v2013-217838
300   $aTitle from title screen (viewed on Aug. 21, 2014).
300   $a"February 2013."
300   $a"Prepared for the 51st Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics, Grapevine, Texas, January 7-10, 2013."
320   $aIncludes bibliographical references (pages 20-21).
606   $aComputational fluid dynamics$2nasat
606   $aShock wave interaction$2nasat
606   $aConvergent-divergent nozzles$2nasat
606   $aSonic booms$2nasat
615  7$aComputational fluid dynamics.
615  7$aShock wave interaction.
615  7$aConvergent-divergent nozzles.
615  7$aSonic booms.
700   $aCastner$b Raymond S.$01392322
702   $aElmiligui$b Alaa
702   $aCliff$b Susan
712 02$aFundamental Aeronautics Program (U.S.)
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704910603321
996   $aExhaust nozzle plume and shock wave interaction$93513071
997   $aUNINA