LEADER 02001nam  2200529Ia 450 
001 9910702114003321
005 20121031073941.0
035   $a(CKB)5470000002425002
035   $a(OCoLC)815517855
035   $a(EXLCZ)995470000002425002
100   $a20121031d2012      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExhaust plume effects on sonic boom for a delta wing and a swept wing-body model$b[electronic resource] /$fRaymond Castner, Troy Lake
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (13 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2012-217446
300   $aTitle from title screen (viewed on Oct. 29, 2012).
300   $a"April 2012."
300   $a"Prepared for the 50th Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics Nashville, Tennessee, January 9-12, 2012."
300   $a"AIAA-2012-1033."
320   $aIncludes bibliographical references (page 13).
606   $aExhaust gases$2nasat
606   $aExhaust nozzles$2nasat
606   $aPressure distribution$2nasat
606   $aSonic booms$2nasat
606   $aBody-wing configurations$2nasat
606   $aPlumes$2nasat
615  7$aExhaust gases.
615  7$aExhaust nozzles.
615  7$aPressure distribution.
615  7$aSonic booms.
615  7$aBody-wing configurations.
615  7$aPlumes.
700   $aCastner$b Raymond$01413911
701   $aLake$b Troy$01413912
712 02$aNASA Glenn Research Center.
712 12$aAIAA Aerospace Sciences Meeting$d(50th :$f2012 :$eNashville, Tenn.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702114003321
996   $aExhaust plume effects on sonic boom for a delta wing and a swept wing-body model$93511556
997   $aUNINA