LEADER 02111nam  2200541 a 450 
001 9910700977903321
005 20111101121516.0
035   $a(CKB)5470000002413246
035   $a(OCoLC)759173412
035   $a(EXLCZ)995470000002413246
100   $a20111101d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aFlow field characterization of an angled supersonic jet near a bluff body$b[electronic resource] /$fJohn D. Wolter ... [and others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011]
215   $a1 online resource (17 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2011-216958
300   $aTitle from title screen (viewed on Nov. 1, 2011).
300   $a"March 2011."
300   $a"Prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 2010."
300   $a"AIAA-2010-4829."
320   $aIncludes bibliographical references (page 17).
606   $aComputational fluid dynamics$2nasat
606   $aTurbulence models$2nasat
606   $aSupersonic jet flow$2nasat
606   $aHigh temperature environments$2nasat
606   $aParticle image velocimetry$2nasat
606   $aFlow distribution$2nasat
606   $aCross flow$2nasat
615  7$aComputational fluid dynamics.
615  7$aTurbulence models.
615  7$aSupersonic jet flow.
615  7$aHigh temperature environments.
615  7$aParticle image velocimetry.
615  7$aFlow distribution.
615  7$aCross flow.
701   $aWolter$b John D$01401710
712 02$aNASA Glenn Research Center.
712 12$aAIAA Applied Aerodynamics Conference$d(28th :$f2010 :$eChicago, Ill.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700977903321
996   $aFlow field characterization of an angled supersonic jet near a bluff body$93470770
997   $aUNINA