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100   $a20100618d2009      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental investigation of the application of microramp flow control to an oblique shock interaction$b[electronic resource] /$fStefanie M. Hirt and Bernhard H. Anderson ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2009]
215   $a1 online resource (27 pages) $cillustrations
225 1 $aNASA TM- ;$v2009-215630
300   $aTitle from title screen (viewed on June 17, 2010).
300   $a"November 2009."
300   $a"AIAA-2009-919."
320   $aIncludes bibliographical references (page 7).
410  0$aNASA technical memorandum ;$v2009-215630.
606   $aOblique shock waves$2nasat
606   $aBoundary layers$2nasat
606   $aShock wave interaction$2nasat
606   $aExperiment design$2nasat
606   $aFactorial design$2nasat
615  7$aOblique shock waves.
615  7$aBoundary layers.
615  7$aShock wave interaction.
615  7$aExperiment design.
615  7$aFactorial design.
700   $aHirt$b Stefanie M$01386037
701   $aAnderson$b Bernhard H$01386038
712 02$aNASA Glenn Research Center.
712 12$aAIAA Aerospace Sciences Meeting$d(47th :$f2009 :$eOrlando, Fla.)
712 12$aAIAA Aerospace Sciences Meeting.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910696924503321
996   $aExperimental investigation of the application of microramp flow control to an oblique shock interaction$93434603
997   $aUNINA