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100   $a20120830d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExhaust nozzle plume effects on sonic boom test results for isolated nozzles$b[electronic resource] /$fRaymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011]
215   $a1 online resource (16 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-217137
300   $aTitle from title screen (viewed on Aug. 30, 2012).
300   $a"December 2011."
300   $a"AIAA-2010-4936."
320   $aIncludes bibliographical references (page 16).
606   $aExhaust nozzles$2nasat
606   $aNozzle flow$2nasat
606   $aPlumes$2nasat
606   $aSupersonic aircraft$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aNozzle geometry$2nasat
606   $aPressure ratio$2nasat
606   $aShock waves$2nasat
606   $aElastic waves$2nasat
615  7$aExhaust nozzles.
615  7$aNozzle flow.
615  7$aPlumes.
615  7$aSupersonic aircraft.
615  7$aComputational fluid dynamics.
615  7$aNozzle geometry.
615  7$aPressure ratio.
615  7$aShock waves.
615  7$aElastic waves.
700   $aCastner$b Raymond S$01392322
712 02$aNASA Glenn Research Center.
712 12$aAIAA Applied Aerodynamics Conference$d(18th :$f2010 :$eChicago, Ill.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701912103321
996   $aExhaust nozzle plume effects on sonic boom test results for isolated nozzles$93518430
997   $aUNINA