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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$aExhaust nozzle plume effects on sonic boom test results for vectored nozzles$b[electronic resource] /$fRaymond Castner
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (16 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217229
300   $aTitle from title screen (viewed on Nov. 1, 2012).
300   $a"February 2012."
300   $a"Prepared for the 47th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE,San Diego, California, July 31-August 3, 2011."
300   $a"AIAA-2011-5974."
320   $aIncludes bibliographical references (pages 15-16).
606   $aExhaust nozzles$2nasat
606   $aSonic booms$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aElastic waves$2nasat
606   $aPlumes$2nasat
606   $aF-15 aircraft$2nasat
606   $aSupersonic aircraft$2nasat
606   $aPressure ratio$2nasat
615  7$aExhaust nozzles.
615  7$aSonic booms.
615  7$aComputational fluid dynamics.
615  7$aElastic waves.
615  7$aPlumes.
615  7$aF-15 aircraft.
615  7$aSupersonic aircraft.
615  7$aPressure ratio.
700   $aCastner$b Raymond S$01392322
712 02$aNASA Glenn Research Center.
712 12$aJoint Propulsion Conference and Exhibit$d(47th :$f2011 :$eSan Diego, Calif.)
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