LEADER 02067nam 2200505Ia 450 001 9910702236603321 005 20121106123957.0 035 $a(CKB)5470000002425784 035 $a(OCoLC)816079914 035 $a(EXLCZ)995470000002425784 100 $a20121106d2012 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aMicro-ramp flow control for oblique shock interactions$b[electronic resource] $ecomparisons of computational and experimental data /$fStefanie M. Hirt, David B. Reich, Michael B. O'Connor 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012] 215 $a1 online resource (14 pages) $cillustrations (some color) 225 1 $aNASA/TM ;$v2012-217242 300 $aTitle from title screen (viewed on Nov. 6, 2012). 300 $a"August 2012." 300 $a"Prepared for the 40th Fluid Dynamics Conference and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 2010." 300 $a"AIAA-2010-4973." 320 $aIncludes bibliographical references (page 14). 517 $aMicro-ramp flow control for oblique shock interactions 606 $aVortex generators$2nasat 606 $aComputational fluid dynamics$2nasat 606 $aOblique shock waves$2nasat 606 $aFlow distribution$2nasat 615 7$aVortex generators. 615 7$aComputational fluid dynamics. 615 7$aOblique shock waves. 615 7$aFlow distribution. 700 $aHirt$b Stefanie M$01386037 701 $aReich$b David B$01388273 701 $aO'Connor$b Michael B$0284913 712 02$aNASA Glenn Research Center. 712 12$aAIAA Computational Fluid Dynamics Conference$d(40th :$f2010 :$eChicago, Ill.) 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910702236603321 996 $aMicro-ramp flow control for oblique shock interactions$93438730 997 $aUNINA